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다음 그림은 세 가지 기체 구성과 형상 변수를 지정할 X 좌표이다. 곡률과 기체 윤곽의 급격한 변화를 정의하는 데 사용된 점을 주목하자. 구성 (c)는 모든 속도 영역에서 기체 단독 분석을 설명하려고 예제 1로 선택되었다. 대략적인 축대칭 기체와 곡선형 기체의 아음속 기체 분석을 수행하였다.

 

기체 모델링 (a) 축대칭 기체, (b) 곡선형 기체, (c) 기체 단독 분석

 

X (FT) S (FT2) P (FT) R (FT) ZU (FT) ZL (FT)
0.0 0.0 0.0 0.0 -0.595 -0.595
0.258 0.080 1.00 0.186 -0.476 -0.715
0.589 0.160 1.42 0.286 -0.372 -0.754
1.26 0.323 2.01 0.424 -0.138 -0.805
2.26 0.751 3.08 0.533 0.200 -0.868
2.59 0.883 3.34 0.533 0.334 -0.868
2.93 0.939 3.44 0.533 0.343 -0.868
3.59 1.032 3.61 0.533 0.343 -0.868
4.57 1.032 3.61 0.533 0.343 -0.868
6.26 1.032 3.61 0.533 0.343 -0.868

 

예제 1에서 4가지 해석의 요약은 다음과 같다.

Case No. Configuration Mach No. Comments
1 Body 0.60 축대칭 해
2 Body 0.60 곡선형 해
3 Body 0.9,1.4,2.5 마하 1.4와 2.5에서 초음속 해석
4 Body 2.5 극초음속 해석

 

이 문제는 CASEID, DUMP CASE, SAVE, 및 NEXT CASE  명령어를 사용하는 방법을 보여준다.

 

입력 파일

 $FLTCON
  NMACH = 1.0,
  MACH(1) = 0.60,
  NALPHA = 11.0,
  ALSCHD(1) = -6.0,-4.0,-2.0,0.0,2.0,4.0,8.0,12.0,16.0,20.0,24.0,
  RNNUB=4.28E6,
 $END
 $OPTINS
  SREF = 8.85,
  CBARR = 2.48,
  BLREF = 4.28,
 $END
 $SYNTHS
  XCG = 4.14,
  ZCG = -0.20,
 $END
 $BODY
  NX = 10.0,
  X(1) = 0.0,0.258,0.589,1.260,2.260,2.590,2.930,3.590,4.570,6.260,
  R(1) = 0.0,0.186,0.286,0.424,0.533,0.533,0.533,0.533,0.533,0.533,
  S(1) = 0.0,0.080,0.160,0.323,0.751,0.883,0.939,1.032,1.032,1.032,
  P(1) = 0.0,1.00,1.42,2.01,3.08,3.34,3.44,3.61,3.61,3.61,
 $END
 $BODY
  BNOSE = 1.0,
  BLN = 2.59,
  BLA = 3.67,
 $END
CASEID APPROXIMATE AXISYMMETRIC BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 1
SAVE
DUMP CASE
NEXT CASE
 $BODY ZU(1) = -.595,-.476,-.372,-.138,.200,.334,.343,.343,.343,.343,
       ZL(1) = -.595,-.715,-.754,-.805,-.868,-.868,-.868,-.868,-.868,-.868,
 $END
CASEID ASYMMETRIC (CAMBERED) BODY SOLUTION,EXAMPLE PROBLEM 1,CASE 2
SAVE
NEXT CASE
 $FLTCON
  NMACH = 3.0,
  MACH(1) = 0.9,1.4,2.5,
  RNNUB = 6.4E6,9.96E6,17.0E6,
 $END
SAVE
CASEID ASYMMETRIC (CAMBERED) BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 3
NEXT CASE
 $FLTCON
  NMACH = 1.0,
  MACH(1) = 2.5,
  RNNUB = 17.86E6,
  HYPERS = .TRUE.,
 $END
 $BODY
  DS = 0.0,
 $END
CASEID HYPERSONIC BODY SOLUTION,  EXAMPLE PROBLEM 1, CASE 4
NEXT CASE

 

출력 파일

 

  ****************************************************
  *    USAF STABILITY AND CONTROL  DIGITAL DATCOM    *
  *    PROGRAM REV. JAN 96   DIRECT INQUIRIES TO:    *
  *    WRIGHT LABORATORY  (WL/FIGC)  ATTN: W. BLAKE  *
  *      WRIGHT PATTERSON AFB, OHIO  45433           *
  *    PHONE (513) 255-6764,   FAX (513) 258-4054    *
  ****************************************************
1                         CONERR - INPUT ERROR CHECKING
0 ERROR CODES - N* DENOTES THE NUMBER OF OCCURENCES OF EACH ERROR
0 A - UNKNOWN VARIABLE NAME
0 B - MISSING EQUAL SIGN FOLLOWING VARIABLE NAME
0 C - NON-ARRAY VARIABLE HAS AN ARRAY ELEMENT DESIGNATION - (N)
0 D - NON-ARRAY VARIABLE HAS MULTIPLE VALUES ASSIGNED
0 E - ASSIGNED VALUES EXCEED ARRAY DIMENSION
0 F - SYNTAX ERROR

0******************************  INPUT DATA CARDS  ******************************

  $FLTCON                                                                        
   NMACH = 1.0,                                                                  
   MACH(1) = 0.60,                                                               
   NALPHA = 11.0,                                                                
   ALSCHD(1) = -6.0,-4.0,-2.0,0.0,2.0,4.0,8.0,12.0,16.0,20.0,24.0,               
   RNNUB=4.28E6,                                                                 
  $END                                                                           
  $OPTINS                                                                        
   SREF = 8.85,                                                                  
   CBARR = 2.48,                                                                 
   BLREF = 4.28,                                                                 
  $END                                                                           
  $SYNTHS                                                                        
   XCG = 4.14,                                                                   
   ZCG = -0.20,                                                                  
  $END                                                                           
  $BODY                                                                          
   NX = 10.0,                                                                    
   X(1) = 0.0,0.258,0.589,1.260,2.260,2.590,2.930,3.590,4.570,6.260,             
   R(1) = 0.0,0.186,0.286,0.424,0.533,0.533,0.533,0.533,0.533,0.533,             
   S(1) = 0.0,0.080,0.160,0.323,0.751,0.883,0.939,1.032,1.032,1.032,             
   P(1) = 0.0,1.00,1.42,2.01,3.08,3.34,3.44,3.61,3.61,3.61,                      
  $END                                                                           
  $BODY                                                                          
   BNOSE = 1.0,                                                                  
   BLN = 2.59,                                                                   
   BLA = 3.67,                                                                   
  $END                                                                           
 CASEID APPROXIMATE AXISYMMETRIC BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 1        
 SAVE                                                                            
 DUMP CASE                                                                       
 NEXT CASE                                                                       
  $BODY ZU(1) = -.595,-.476,-.372,-.138,.200,.334,.343,.343,.343,.343,           
        ZL(1) = -.595,-.715,-.754,-.805,-.868,-.868,-.868,-.868,-.868,-.868,     
  $END                                                                           
 CASEID ASYMMETRIC (CAMBERED) BODY SOLUTION,EXAMPLE PROBLEM 1,CASE 2             
 SAVE                                                                            
 NEXT CASE                                                                       
  $FLTCON                                                                        
   NMACH = 3.0,                                                                  
   MACH(1) = 0.9,1.4,2.5,                                                        
   RNNUB = 6.4E6,9.96E6,17.0E6,                                                  
  $END                                                                           
 SAVE                                                                            
 CASEID ASYMMETRIC (CAMBERED) BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 3           
 NEXT CASE                                                                       
  $FLTCON                                                                        
   NMACH = 1.0,                                                                  
   MACH(1) = 2.5,                                                                
   RNNUB = 17.86E6,                                                              
   HYPERS = .TRUE.,                                                              
  $END                                                                           
  $BODY                                                                          
   DS = 0.0,                                                                     
  $END                                                                           
 CASEID HYPERSONIC BODY SOLUTION,  EXAMPLE PROBLEM 1, CASE 4                     
 NEXT CASE                                                                       
1          THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
  $FLTCON                                                                        
   NMACH = 1.0,                                                                  
   MACH(1) = 0.60,                                                               
   NALPHA = 11.0,                                                                
   ALSCHD(1) = -6.0,-4.0,-2.0,0.0,2.0,4.0,8.0,12.0,16.0,20.0,24.0,               
   RNNUB=4.28E6,                                                                 
  $END                                                                           
  $OPTINS                                                                        
   SREF = 8.85,                                                                  
   CBARR = 2.48,                                                                 
   BLREF = 4.28,                                                                 
  $END                                                                           
  $SYNTHS                                                                        
   XCG = 4.14,                                                                   
   ZCG = -0.20,                                                                  
  $END                                                                           
  $BODY                                                                          
   NX = 10.0,                                                                    
   X(1) = 0.0,0.258,0.589,1.260,2.260,2.590,2.930,3.590,4.570,6.260,             
   R(1) = 0.0,0.186,0.286,0.424,0.533,0.533,0.533,0.533,0.533,0.533,             
   S(1) = 0.0,0.080,0.160,0.323,0.751,0.883,0.939,1.032,1.032,1.032,             
   P(1) = 0.0,1.00,1.42,2.01,3.08,3.34,3.44,3.61,3.61,3.61,                      
  $END                                                                           
  $BODY                                                                          
   BNOSE = 1.0,                                                                  
   BLN = 2.59,                                                                   
   BLA = 3.67,                                                                   
  $END                                                                           
 CASEID APPROXIMATE AXISYMMETRIC BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 1        
 SAVE                                                                            
 DUMP CASE                                                                       
 NEXT CASE                                                                       
0 INPUT DIMENSIONS ARE IN FT, SCALE FACTOR IS 1.0000

 
    BD(  1)= 6.26000E+00    BD(  2)= 3.59000E+00    BD(  3)= 1.03200E+00    BD(  4)= 1.03200E+00    BD(  5)= 6.26000E+00
    BD(  6)= 1.03200E+00    BD(  7)= 5.66530E+00    BD(  8)= 1.00000E-30    BD(  9)= 8.43444E-01    BD( 10)= 2.08059E-02
    BD( 11)= 0.00000E+00    BD( 12)= 1.00000E-30    BD( 13)= 1.00000E-30    BD( 14)= 1.00000E-30    BD( 15)= 1.00000E-30
    BD( 16)= 1.00000E-30    BD( 17)= 1.00000E-30    BD( 18)= 1.00000E-30    BD( 19)= 1.00000E-30    BD( 20)= 1.00000E-30
    BD( 21)= 1.00000E-30    BD( 22)= 1.00000E-30    BD( 23)= 1.00000E-30    BD( 24)= 1.00000E-30    BD( 25)= 1.00000E-30
    BD( 26)= 1.00000E-30    BD( 27)= 1.00000E-30    BD( 28)= 1.00000E-30    BD( 29)= 1.00000E-30    BD( 30)= 1.00000E-30
    BD( 31)= 1.00000E-30    BD( 32)= 1.00000E-30    BD( 33)= 4.14000E+00    BD( 34)= 1.00000E-30    BD( 35)= 1.00000E-30
    BD( 36)= 1.00000E-30    BD( 37)= 1.00000E-30    BD( 38)= 1.00000E-30    BD( 39)= 1.00000E-30    BD( 40)= 1.00000E-30
    BD( 41)= 1.00000E-30    BD( 42)= 1.00000E-30    BD( 43)= 1.00000E-30    BD( 44)= 1.00000E-30    BD( 45)= 1.00000E-30
    BD( 46)= 1.00000E-30    BD( 47)= 1.00000E-30    BD( 48)= 1.00000E-30    BD( 49)= 1.00000E-30    BD( 50)= 1.00000E-30
    BD( 51)= 1.00000E-30    BD( 52)= 1.00000E-30    BD( 53)= 1.00000E-30    BD( 54)= 1.00000E-30    BD( 55)= 4.69500E+05
    BD( 56)= 1.03200E+00    BD( 57)= 1.03200E+00    BD( 58)= 1.00000E-30    BD( 59)= 7.12853E-03    BD( 60)= 1.36774E-02
    BD( 61)= 2.08059E-02    BD( 62)= 1.00000E-30    BD( 63)= 1.00000E-30    BD( 64)= 1.00000E-30    BD( 65)= 1.00000E-30
    BD( 66)= 1.00000E-30    BD( 67)= 1.00000E-30    BD( 68)= 1.00000E-30    BD( 69)= 1.00000E-30    BD( 70)= 1.00000E-30
    BD( 71)= 1.00000E-30    BD( 72)= 1.00000E-30    BD( 73)= 1.00000E-30    BD( 74)= 1.00000E-30    BD( 75)= 5.46109E+00
    BD( 76)= 6.21916E-01    BD( 77)= 1.00000E-30    BD( 78)= 1.00000E-30    BD( 79)= 1.00000E-30    BD( 80)= 1.00000E-30
    BD( 81)= 0.00000E+00    BD( 82)=-2.00000E-01    BD( 83)= 2.00000E-30    BD( 84)= 1.00000E-30    BD( 85)= 1.14629E+00
    BD( 86)= 1.14629E+00    BD( 87)= 1.00000E-30    BD( 88)= 0.00000E+00    BD( 89)= 1.00000E-30    BD( 90)= 2.67928E+07
    BD( 91)= 3.79712E+07    BD( 92)= 2.48495E-03    BD( 93)= 1.83698E+01    BD( 94)= 1.10000E+01    BD( 95)= 1.00000E-30
    BD( 96)= 1.00000E-30    BD( 97)= 1.00000E-30    BD( 98)= 1.00000E-30    BD( 99)= 1.00000E-30    BD(100)= 1.00000E-30
    BD(101)= 1.00000E-30    BD(102)= 1.00000E-30    BD(103)= 1.00000E-30    BD(104)= 1.00000E-30    BD(105)= 1.00000E-30
    BD(106)= 1.00000E-30    BD(107)= 1.00000E-30    BD(108)= 1.00000E-30    BD(109)= 1.00000E-30    BD(110)= 1.00000E-30
    BD(111)= 1.00000E-30    BD(112)= 1.00000E-30    BD(113)= 1.00000E-30    BD(114)= 1.00000E-30    BD(115)= 1.00000E-30
    BD(116)= 1.00000E-30    BD(117)= 1.00000E-30    BD(118)= 1.00000E-30    BD(119)= 1.00000E-30    BD(120)= 1.00000E-30
    BD(121)= 1.00000E-30    BD(122)= 1.00000E-30    BD(123)= 1.00000E-30    BD(124)= 1.00000E-30    BD(125)= 1.00000E-30
    BD(126)= 1.00000E-30    BD(127)= 1.00000E-30    BD(128)= 1.00000E-30    BD(129)= 1.00000E-30    BD(130)= 1.00000E-30
    BD(131)= 1.00000E-30    BD(132)= 1.00000E-30    BD(133)= 1.00000E-30    BD(134)= 1.00000E-30    BD(135)= 1.20000E+00
    BD(136)= 1.20000E+00    BD(137)= 1.20000E+00    BD(138)= 1.20000E+00    BD(139)= 1.20000E+00    BD(140)= 1.20000E+00
    BD(141)= 1.20000E+00    BD(142)= 1.20000E+00    BD(143)= 1.20000E+00    BD(144)= 1.20052E+00    BD(145)= 1.20440E+00
    BD(146)= 1.00000E-30    BD(147)= 1.00000E-30    BD(148)= 1.00000E-30    BD(149)= 1.00000E-30    BD(150)= 1.00000E-30
    BD(151)= 1.00000E-30    BD(152)= 1.00000E-30    BD(153)= 1.00000E-30    BD(154)= 1.00000E-30    BD(155)=-2.05992E-02
    BD(156)=-1.37328E-02    BD(157)=-6.86641E-03    BD(158)= 0.00000E+00    BD(159)= 6.86641E-03    BD(160)= 1.37328E-02
    BD(161)= 2.74656E-02    BD(162)= 4.11985E-02    BD(163)= 5.49313E-02    BD(164)= 6.86641E-02    BD(165)= 8.23969E-02
    BD(166)= 1.00000E-30    BD(167)= 1.00000E-30    BD(168)= 1.00000E-30    BD(169)= 1.00000E-30    BD(170)= 1.00000E-30
    BD(171)= 1.00000E-30    BD(172)= 1.00000E-30    BD(173)= 1.00000E-30    BD(174)= 1.00000E-30    BD(175)= 1.00000E-30
    BD(176)= 1.00000E-30    BD(177)= 1.00000E-30    BD(178)= 1.00000E-30    BD(179)= 1.00000E-30    BD(180)= 1.00000E-30
    BD(181)= 1.00000E-30    BD(182)= 1.00000E-30    BD(183)= 1.00000E-30    BD(184)= 1.00000E-30    BD(185)= 1.00000E-30
    BD(186)= 1.00000E-30    BD(187)= 1.00000E-30    BD(188)= 1.00000E-30    BD(189)= 1.00000E-30    BD(190)= 1.00000E-30
    BD(191)= 1.00000E-30    BD(192)= 1.00000E-30    BD(193)= 1.00000E-30    BD(194)= 1.00000E-30    BD(195)=-0.00000E+00
    BD(196)=-0.00000E+00    BD(197)=-0.00000E+00    BD(198)= 0.00000E+00    BD(199)= 0.00000E+00    BD(200)= 0.00000E+00
    BD(201)= 0.00000E+00    BD(202)= 0.00000E+00    BD(203)= 0.00000E+00    BD(204)= 0.00000E+00    BD(205)= 0.00000E+00
    BD(206)= 1.00000E-30    BD(207)= 1.00000E-30    BD(208)= 1.00000E-30    BD(209)= 1.00000E-30    BD(210)= 1.00000E-30
    BD(211)= 1.00000E-30    BD(212)= 1.00000E-30    BD(213)= 1.00000E-30    BD(214)= 1.00000E-30    BD(215)= 2.15321E-03
    BD(216)= 9.57953E-04    BD(217)= 2.39634E-04    BD(218)= 0.00000E+00    BD(219)= 2.39634E-04    BD(220)= 9.57953E-04
    BD(221)= 3.82248E-03    BD(222)= 8.56564E-03    BD(223)= 1.51411E-02    BD(224)= 2.34845E-02    BD(225)= 3.35139E-02
    BD(226)= 1.00000E-30    BD(227)= 1.00000E-30    BD(228)= 1.00000E-30    BD(229)= 1.00000E-30    BD(230)= 1.00000E-30
    BD(231)= 1.00000E-30    BD(232)= 1.00000E-30    BD(233)= 1.00000E-30    BD(234)= 1.00000E-30    BD(235)= 1.00000E-30
    BD(236)= 1.00000E-30    BD(237)= 1.00000E-30    BD(238)= 1.00000E-30    BD(239)= 1.00000E-30    BD(240)= 1.00000E-30
    BD(241)= 1.00000E-30    BD(242)= 1.00000E-30    BD(243)= 1.00000E-30    BD(244)= 1.00000E-30    BD(245)= 1.00000E-30
    BD(246)= 1.00000E-30    BD(247)= 1.00000E-30    BD(248)= 1.00000E-30    BD(249)= 1.00000E-30    BD(250)= 1.00000E-30
    BD(251)= 1.00000E-30    BD(252)= 1.00000E-30    BD(253)= 1.00000E-30    BD(254)= 1.00000E-30    BD(255)=-6.00000E+00
    BD(256)=-4.00000E+00    BD(257)=-2.00000E+00    BD(258)= 0.00000E+00    BD(259)= 2.00000E+00    BD(260)= 4.00000E+00
    BD(261)= 8.00000E+00    BD(262)= 1.20000E+01    BD(263)= 1.60000E+01    BD(264)= 2.00000E+01    BD(265)= 2.40000E+01
    BD(266)= 1.00000E-30    BD(267)= 1.00000E-30    BD(268)= 1.00000E-30    BD(269)= 1.00000E-30    BD(270)= 1.00000E-30
    BD(271)= 1.00000E-30    BD(272)= 1.00000E-30    BD(273)= 1.00000E-30    BD(274)= 1.00000E-30    BD(275)= 1.00000E-30
    BD(276)= 1.00000E-30    BD(277)= 1.00000E-30    BD(278)= 1.00000E-30    BD(279)= 1.00000E-30    BD(280)= 1.00000E-30
    BD(281)= 1.00000E-30    BD(282)= 1.00000E-30    BD(283)= 1.00000E-30    BD(284)= 1.00000E-30    BD(285)= 1.00000E-30
    BD(286)= 1.00000E-30    BD(287)= 1.00000E-30    BD(288)= 1.00000E-30    BD(289)= 1.00000E-30    BD(290)= 1.00000E-30
    BD(291)= 1.00000E-30    BD(292)= 1.00000E-30    BD(293)= 1.00000E-30    BD(294)= 1.00000E-30    BD(295)= 1.00000E-30
    BD(296)= 1.00000E-30    BD(297)= 1.00000E-30    BD(298)= 1.00000E-30    BD(299)= 1.00000E-30    BD(300)= 1.00000E-30
    BD(301)= 1.00000E-30    BD(302)= 1.00000E-30    BD(303)= 1.00000E-30    BD(304)= 1.00000E-30    BD(305)= 1.00000E-30
    BD(306)= 1.00000E-30    BD(307)= 1.00000E-30    BD(308)= 1.00000E-30    BD(309)= 1.00000E-30    BD(310)= 1.00000E-30
    BD(311)= 1.00000E-30    BD(312)= 1.00000E-30    BD(313)= 1.00000E-30    BD(314)= 1.00000E-30    BD(315)= 1.00000E-30
    BD(316)= 1.00000E-30    BD(317)= 1.00000E-30    BD(318)= 1.00000E-30    BD(319)= 1.00000E-30    BD(320)= 1.00000E-30
    BD(321)= 1.00000E-30    BD(322)= 1.00000E-30    BD(323)= 1.00000E-30    BD(324)= 1.00000E-30    BD(325)= 1.00000E-30
    BD(326)= 1.00000E-30    BD(327)= 1.00000E-30    BD(328)= 1.00000E-30    BD(329)= 1.00000E-30    BD(330)= 1.00000E-30
    BD(331)= 1.00000E-30    BD(332)= 1.00000E-30    BD(333)= 1.00000E-30    BD(334)= 1.00000E-30    BD(335)= 1.00000E-30
    BD(336)= 1.00000E-30    BD(337)= 1.00000E-30    BD(338)= 1.00000E-30    BD(339)= 1.00000E-30    BD(340)= 1.00000E-30
    BD(341)= 1.00000E-30    BD(342)= 1.00000E-30    BD(343)= 1.00000E-30    BD(344)= 1.00000E-30    BD(345)= 1.00000E-30
    BD(346)= 1.00000E-30    BD(347)= 1.00000E-30    BD(348)= 1.00000E-30    BD(349)= 1.00000E-30    BD(350)= 1.00000E-30
    BD(351)= 1.00000E-30    BD(352)= 1.00000E-30    BD(353)= 1.00000E-30    BD(354)= 1.00000E-30    BD(355)= 1.00000E-30
    BD(356)= 1.00000E-30    BD(357)= 1.00000E-30    BD(358)= 1.00000E-30    BD(359)= 1.00000E-30    BD(360)= 1.00000E-30
    BD(361)= 1.00000E-30    BD(362)= 1.00000E-30    BD(363)= 1.00000E-30    BD(364)= 1.00000E-30    BD(365)= 1.00000E-30
    BD(366)= 1.00000E-30    BD(367)= 1.00000E-30    BD(368)= 1.00000E-30    BD(369)= 1.00000E-30    BD(370)= 1.00000E-30
    BD(371)= 1.00000E-30    BD(372)= 1.00000E-30    BD(373)= 1.00000E-30    BD(374)= 1.00000E-30    BD(375)= 1.00000E-30
    BD(376)= 1.00000E-30    BD(377)= 1.00000E-30    BD(378)= 1.00000E-30    BD(379)= 1.00000E-30    BD(380)= 1.00000E-30
    BD(381)= 1.00000E-30    BD(382)= 1.00000E-30    BD(383)= 1.00000E-30    BD(384)= 1.00000E-30    BD(385)= 1.00000E-30
    BD(386)= 1.00000E-30    BD(387)= 1.00000E-30    BD(388)= 1.00000E-30    BD(389)= 1.00000E-30    BD(390)= 1.00000E-30
    BD(391)= 1.00000E-30    BD(392)= 1.00000E-30    BD(393)= 1.00000E-30    BD(394)= 1.00000E-30    BD(395)= 1.00000E-30
    BD(396)= 1.00000E-30    BD(397)= 1.00000E-30    BD(398)= 1.00000E-30    BD(399)= 1.00000E-30    BD(400)= 1.00000E-30
    BD(401)= 1.00000E-30    BD(402)= 1.00000E-30    BD(403)= 1.00000E-30    BD(404)= 1.00000E-30    BD(405)= 1.00000E-30
    BD(406)= 1.00000E-30    BD(407)= 1.00000E-30    BD(408)= 1.00000E-30    BD(409)= 1.00000E-30    BD(410)= 1.00000E-30
    BD(411)= 1.00000E-30    BD(412)= 1.00000E-30    BD(413)= 1.00000E-30    BD(414)= 1.00000E-30    BD(415)= 1.00000E-30
    BD(416)= 1.00000E-30    BD(417)= 1.00000E-30    BD(418)= 1.00000E-30    BD(419)= 1.00000E-30    BD(420)= 1.00000E-30
    BD(421)= 1.00000E-30    BD(422)= 1.00000E-30    BD(423)= 1.00000E-30    BD(424)= 1.00000E-30    BD(425)= 1.00000E-30
    BD(426)= 1.00000E-30    BD(427)= 1.00000E-30    BD(428)= 1.00000E-30    BD(429)= 1.00000E-30    BD(430)= 1.00000E-30
    BD(431)= 1.00000E-30    BD(432)= 1.00000E-30    BD(433)= 1.00000E-30    BD(434)= 1.00000E-30    BD(435)= 1.00000E-30
    BD(436)= 1.00000E-30    BD(437)= 1.00000E-30    BD(438)= 1.00000E-30    BD(439)= 1.00000E-30    BD(440)= 1.00000E-30
    BD(441)= 1.00000E-30    BD(442)= 1.00000E-30    BD(443)= 1.00000E-30    BD(444)= 1.00000E-30    BD(445)= 1.00000E-30
    BD(446)= 1.00000E-30    BD(447)= 1.00000E-30    BD(448)= 1.00000E-30    BD(449)= 1.00000E-30    BD(450)= 1.00000E-30
    BD(451)= 1.00000E-30    BD(452)= 1.00000E-30    BD(453)= 1.00000E-30    BD(454)= 1.00000E-30    BD(455)= 1.00000E-30
    BD(456)= 1.00000E-30    BD(457)= 1.00000E-30    BD(458)= 1.00000E-30    BD(459)= 1.00000E-30    BD(460)= 1.00000E-30
    BD(461)= 1.00000E-30    BD(462)= 1.00000E-30    BD(463)= 1.00000E-30    BD(464)= 1.00000E-30    BD(465)= 1.00000E-30
    BD(466)= 1.00000E-30    BD(467)= 1.00000E-30    BD(468)= 1.00000E-30    BD(469)= 1.00000E-30    BD(470)= 1.00000E-30
    BD(471)= 1.00000E-30    BD(472)= 1.00000E-30    BD(473)= 1.00000E-30    BD(474)= 1.00000E-30    BD(475)= 1.00000E-30
    BD(476)= 1.00000E-30    BD(477)= 1.00000E-30    BD(478)= 1.00000E-30    BD(479)= 1.00000E-30    BD(480)= 1.00000E-30
    BD(481)= 1.00000E-30    BD(482)= 1.00000E-30    BD(483)= 1.00000E-30    BD(484)= 1.00000E-30    BD(485)= 1.00000E-30
    BD(486)= 1.00000E-30    BD(487)= 1.00000E-30    BD(488)= 1.00000E-30    BD(489)= 1.00000E-30    BD(490)= 1.00000E-30
    BD(491)= 1.00000E-30    BD(492)= 1.00000E-30    BD(493)= 1.00000E-30    BD(494)= 1.00000E-30    BD(495)= 1.00000E-30
    BD(496)= 1.00000E-30    BD(497)= 1.00000E-30    BD(498)= 1.00000E-30    BD(499)= 1.00000E-30    BD(500)= 1.00000E-30
    BD(501)= 1.00000E-30    BD(502)= 1.00000E-30    BD(503)= 1.00000E-30    BD(504)= 1.00000E-30    BD(505)= 1.00000E-30
    BD(506)= 1.00000E-30    BD(507)= 1.00000E-30    BD(508)= 1.00000E-30    BD(509)= 1.00000E-30    BD(510)= 1.00000E-30
    BD(511)= 1.00000E-30    BD(512)= 1.00000E-30    BD(513)= 1.00000E-30    BD(514)= 1.00000E-30    BD(515)= 1.00000E-30
    BD(516)= 1.00000E-30    BD(517)= 1.00000E-30    BD(518)= 1.00000E-30    BD(519)= 1.00000E-30    BD(520)= 1.00000E-30
    BD(521)= 1.00000E-30    BD(522)= 1.00000E-30    BD(523)= 1.00000E-30    BD(524)= 1.00000E-30    BD(525)= 1.00000E-30
    BD(526)= 1.00000E-30    BD(527)= 1.00000E-30    BD(528)= 1.00000E-30    BD(529)= 1.00000E-30    BD(530)= 1.00000E-30
    BD(531)= 1.00000E-30    BD(532)= 1.00000E-30    BD(533)= 1.00000E-30    BD(534)= 1.00000E-30    BD(535)= 1.00000E-30
    BD(536)= 1.00000E-30    BD(537)= 1.00000E-30    BD(538)= 1.00000E-30    BD(539)= 1.00000E-30    BD(540)= 1.00000E-30
    BD(541)= 1.00000E-30    BD(542)= 1.00000E-30    BD(543)= 1.00000E-30    BD(544)= 1.00000E-30    BD(545)= 1.00000E-30
    BD(546)= 1.00000E-30    BD(547)= 1.00000E-30    BD(548)= 1.00000E-30    BD(549)= 1.00000E-30    BD(550)= 1.00000E-30
    BD(551)= 1.00000E-30    BD(552)= 1.00000E-30    BD(553)= 1.00000E-30    BD(554)= 1.00000E-30    BD(555)= 1.00000E-30
    BD(556)= 1.00000E-30    BD(557)= 1.00000E-30    BD(558)= 1.00000E-30    BD(559)= 1.00000E-30    BD(560)= 1.00000E-30
    BD(561)= 1.00000E-30    BD(562)= 1.00000E-30    BD(563)= 1.00000E-30    BD(564)= 1.00000E-30    BD(565)= 1.00000E-30
    BD(566)= 1.00000E-30    BD(567)= 1.00000E-30    BD(568)= 1.00000E-30    BD(569)= 1.00000E-30    BD(570)= 1.00000E-30
    BD(571)= 1.00000E-30    BD(572)= 1.00000E-30    BD(573)= 1.00000E-30    BD(574)= 1.00000E-30    BD(575)= 1.00000E-30
    BD(576)= 1.00000E-30    BD(577)= 1.00000E-30    BD(578)= 1.00000E-30    BD(579)= 1.00000E-30    BD(580)= 1.00000E-30
    BD(581)= 1.00000E-30    BD(582)= 1.00000E-30    BD(583)= 1.00000E-30    BD(584)= 1.00000E-30    BD(585)= 1.00000E-30
    BD(586)= 1.00000E-30    BD(587)= 1.00000E-30    BD(588)= 1.00000E-30    BD(589)= 1.00000E-30    BD(590)= 1.00000E-30
    BD(591)= 1.00000E-30    BD(592)= 1.00000E-30    BD(593)= 1.00000E-30    BD(594)= 1.00000E-30    BD(595)= 1.00000E-30
    BD(596)= 1.00000E-30    BD(597)= 1.00000E-30    BD(598)= 1.00000E-30    BD(599)= 1.00000E-30    BD(600)= 1.00000E-30
    BD(601)= 1.00000E-30    BD(602)= 1.00000E-30    BD(603)= 1.00000E-30    BD(604)= 1.00000E-30    BD(605)= 1.00000E-30
    BD(606)= 1.00000E-30    BD(607)= 1.00000E-30    BD(608)= 1.00000E-30    BD(609)= 1.00000E-30    BD(610)= 1.00000E-30
    BD(611)= 1.00000E-30    BD(612)= 1.00000E-30    BD(613)= 1.00000E-30    BD(614)= 1.00000E-30    BD(615)= 1.00000E-30
    BD(616)= 1.00000E-30    BD(617)= 1.00000E-30    BD(618)= 1.00000E-30    BD(619)= 1.00000E-30    BD(620)= 1.00000E-30
    BD(621)= 1.00000E-30    BD(622)= 1.00000E-30    BD(623)= 1.00000E-30    BD(624)= 1.00000E-30    BD(625)= 1.00000E-30
    BD(626)= 1.00000E-30    BD(627)= 1.00000E-30    BD(628)= 1.00000E-30    BD(629)= 1.00000E-30    BD(630)= 1.00000E-30
    BD(631)= 1.00000E-30    BD(632)= 1.00000E-30    BD(633)= 1.00000E-30    BD(634)= 1.00000E-30    BD(635)= 1.00000E-30
    BD(636)= 1.00000E-30    BD(637)= 1.00000E-30    BD(638)= 1.00000E-30    BD(639)= 1.00000E-30    BD(640)= 1.00000E-30
    BD(641)= 1.00000E-30    BD(642)= 1.00000E-30    BD(643)= 1.00000E-30    BD(644)= 1.00000E-30    BD(645)= 1.00000E-30
    BD(646)= 1.00000E-30    BD(647)= 1.00000E-30    BD(648)= 1.00000E-30    BD(649)= 1.00000E-30    BD(650)= 1.00000E-30
    BD(651)= 1.00000E-30    BD(652)= 1.00000E-30    BD(653)= 1.00000E-30    BD(654)= 1.00000E-30    BD(655)= 1.00000E-30
    BD(656)= 1.00000E-30    BD(657)= 1.00000E-30    BD(658)= 1.00000E-30    BD(659)= 1.00000E-30    BD(660)= 1.00000E-30
    BD(661)= 1.00000E-30    BD(662)= 1.00000E-30    BD(663)= 1.00000E-30    BD(664)= 1.00000E-30    BD(665)= 1.00000E-30
    BD(666)= 1.00000E-30    BD(667)= 1.00000E-30    BD(668)= 1.00000E-30    BD(669)= 1.00000E-30    BD(670)= 1.00000E-30
    BD(671)= 1.00000E-30    BD(672)= 1.00000E-30    BD(673)= 1.00000E-30    BD(674)= 1.00000E-30    BD(675)= 1.00000E-30
    BD(676)= 1.00000E-30    BD(677)= 1.00000E-30    BD(678)= 1.00000E-30    BD(679)= 1.00000E-30    BD(680)= 1.00000E-30
    BD(681)= 1.00000E-30    BD(682)= 1.00000E-30    BD(683)= 1.00000E-30    BD(684)= 1.00000E-30    BD(685)= 1.00000E-30
    BD(686)= 1.00000E-30    BD(687)= 1.00000E-30    BD(688)= 1.00000E-30    BD(689)= 1.00000E-30    BD(690)= 1.00000E-30
    BD(691)= 1.00000E-30    BD(692)= 1.00000E-30    BD(693)= 1.00000E-30    BD(694)= 1.00000E-30    BD(695)= 1.00000E-30
    BD(696)= 1.00000E-30    BD(697)= 1.00000E-30    BD(698)= 1.00000E-30    BD(699)= 1.00000E-30    BD(700)= 1.00000E-30
    BD(701)= 1.00000E-30    BD(702)= 1.00000E-30    BD(703)= 1.00000E-30    BD(704)= 1.00000E-30    BD(705)= 1.00000E-30
    BD(706)= 1.00000E-30    BD(707)= 1.00000E-30    BD(708)= 1.00000E-30    BD(709)= 1.00000E-30    BD(710)= 1.00000E-30
    BD(711)= 1.00000E-30    BD(712)= 1.00000E-30    BD(713)= 1.00000E-30    BD(714)= 1.00000E-30    BD(715)= 1.00000E-30
    BD(716)= 1.00000E-30    BD(717)= 1.00000E-30    BD(718)= 1.00000E-30    BD(719)= 1.00000E-30    BD(720)= 1.00000E-30
    BD(721)= 1.00000E-30    BD(722)= 1.00000E-30    BD(723)= 1.00000E-30    BD(724)= 1.00000E-30    BD(725)= 1.00000E-30
    BD(726)= 1.00000E-30    BD(727)= 1.00000E-30    BD(728)= 1.00000E-30    BD(729)= 1.00000E-30    BD(730)= 1.00000E-30
    BD(731)= 1.00000E-30    BD(732)= 1.00000E-30    BD(733)= 1.00000E-30    BD(734)= 1.00000E-30    BD(735)= 1.00000E-30
    BD(736)= 1.00000E-30    BD(737)= 1.00000E-30    BD(738)= 1.00000E-30    BD(739)= 1.00000E-30    BD(740)= 1.00000E-30
    BD(741)= 1.00000E-30    BD(742)= 1.00000E-30    BD(743)= 1.00000E-30    BD(744)= 1.00000E-30    BD(745)= 1.00000E-30
    BD(746)= 1.00000E-30    BD(747)= 1.00000E-30    BD(748)= 1.00000E-30    BD(749)= 1.00000E-30    BD(750)= 1.00000E-30
    BD(751)= 1.00000E-30    BD(752)= 1.00000E-30    BD(753)= 1.00000E-30    BD(754)= 1.00000E-30    BD(755)= 1.00000E-30
    BD(756)= 1.00000E-30    BD(757)= 1.00000E-30    BD(758)= 1.00000E-30    BD(759)= 1.00000E-30    BD(760)= 1.00000E-30
    BD(761)= 1.00000E-30    BD(762)= 1.00000E-30
 
   STB(  1)= 1.00000E-30   STB(  2)= 0.00000E+00   STB(  3)= 1.00000E+00   STB(  4)= 1.00000E-30   STB(  5)= 1.00000E-30
   STB(  6)= 1.00000E-30   STB(  7)= 1.00000E-30   STB(  8)= 1.00000E-30   STB(  9)= 1.00000E-30   STB( 10)= 1.00000E-30
   STB( 11)= 1.00000E-30   STB( 12)= 1.00000E-30   STB( 13)= 1.00000E-30   STB( 14)= 1.00000E-30   STB( 15)= 1.00000E-30
   STB( 16)= 1.00000E-30   STB( 17)= 1.00000E-30   STB( 18)= 1.00000E-30   STB( 19)= 1.00000E-30   STB( 20)= 1.00000E-30
   STB( 21)= 1.00000E-30   STB( 22)= 1.00000E-30   STB( 23)= 1.00000E-30   STB( 24)= 1.00000E-30   STB( 25)= 1.00000E-30
   STB( 26)= 1.00000E-30   STB( 27)= 1.00000E-30   STB( 28)= 1.00000E-30   STB( 29)= 1.00000E-30   STB( 30)= 1.00000E-30
   STB( 31)= 1.00000E-30   STB( 32)= 1.00000E-30   STB( 33)= 1.00000E-30   STB( 34)= 1.00000E-30   STB( 35)= 1.00000E-30
   STB( 36)= 1.00000E-30   STB( 37)= 1.00000E-30   STB( 38)= 1.00000E-30   STB( 39)= 1.00000E-30   STB( 40)= 1.00000E-30
   STB( 41)= 1.00000E-30   STB( 42)= 1.00000E-30   STB( 43)= 1.00000E-30   STB( 44)= 1.00000E-30   STB( 45)= 1.00000E-30
   STB( 46)= 1.00000E-30   STB( 47)= 1.00000E-30   STB( 48)= 1.00000E-30   STB( 49)= 1.00000E-30   STB( 50)= 1.00000E-30
   STB( 51)= 1.00000E-30   STB( 52)= 1.00000E-30   STB( 53)= 1.00000E-30   STB( 54)= 1.00000E-30   STB( 55)= 1.00000E-30
   STB( 56)= 1.00000E-30   STB( 57)= 1.00000E-30   STB( 58)= 1.00000E-30   STB( 59)= 1.00000E-30   STB( 60)= 1.00000E-30
   STB( 61)= 1.00000E-30   STB( 62)= 1.00000E-30   STB( 63)= 1.00000E-30   STB( 64)= 1.00000E-30   STB( 65)= 1.00000E-30
   STB( 66)= 1.00000E-30   STB( 67)= 1.00000E-30   STB( 68)= 1.00000E-30   STB( 69)= 1.00000E-30   STB( 70)= 1.00000E-30
   STB( 71)= 1.00000E-30   STB( 72)= 1.00000E-30   STB( 73)= 1.00000E-30   STB( 74)= 1.00000E-30   STB( 75)= 1.00000E-30
   STB( 76)= 1.00000E-30   STB( 77)= 1.00000E-30   STB( 78)= 1.00000E-30   STB( 79)= 1.00000E-30   STB( 80)= 1.00000E-30
   STB( 81)= 1.00000E-30   STB( 82)= 1.00000E-30   STB( 83)= 1.00000E-30   STB( 84)= 1.00000E-30   STB( 85)= 1.00000E-30
   STB( 86)= 1.00000E-30   STB( 87)= 1.00000E-30   STB( 88)= 1.00000E-30   STB( 89)= 1.00000E-30   STB( 90)= 1.00000E-30
   STB( 91)= 1.00000E-30   STB( 92)= 1.00000E-30   STB( 93)= 1.00000E-30   STB( 94)= 1.00000E-30   STB( 95)= 1.00000E-30
   STB( 96)= 1.00000E-30   STB( 97)= 1.00000E-30   STB( 98)= 1.00000E-30   STB( 99)= 1.00000E-30   STB(100)= 1.00000E-30
   STB(101)= 1.00000E-30   STB(102)= 1.00000E-30   STB(103)= 1.00000E-30   STB(104)= 1.00000E-30   STB(105)= 1.00000E-30
   STB(106)= 1.00000E-30   STB(107)= 1.00000E-30   STB(108)= 1.00000E-30   STB(109)= 1.00000E-30   STB(110)= 1.00000E-30
   STB(111)= 1.00000E-30   STB(112)= 1.00000E-30   STB(113)= 1.00000E-30   STB(114)= 1.00000E-30   STB(115)= 1.00000E-30
   STB(116)= 1.00000E-30   STB(117)= 1.00000E-30   STB(118)= 1.00000E-30   STB(119)= 1.00000E-30   STB(120)= 1.00000E-30
   STB(121)= 1.00000E-30   STB(122)= 1.00000E-30   STB(123)= 1.00000E-30   STB(124)= 1.00000E-30   STB(125)= 1.00000E-30
   STB(126)= 1.00000E-30   STB(127)= 1.00000E-30   STB(128)= 1.00000E-30   STB(129)= 1.00000E-30   STB(130)= 1.00000E-30
   STB(131)= 1.00000E-30   STB(132)= 1.00000E-30   STB(133)= 1.00000E-30   STB(134)= 1.00000E-30   STB(135)= 1.00000E-30
0**** FOLLOWING ARE THE BASIC INPUT DATA BLOCKS ****
 
   FLC(  1)= 1.00000E+00   FLC(  2)= 1.10000E+01   FLC(  3)= 6.00000E-01   FLC(  4)= 1.00000E-30   FLC(  5)= 1.00000E-30
   FLC(  6)= 1.00000E-30   FLC(  7)= 1.00000E-30   FLC(  8)= 1.00000E-30   FLC(  9)= 1.00000E-30   FLC( 10)= 1.00000E-30
   FLC( 11)= 1.00000E-30   FLC( 12)= 1.00000E-30   FLC( 13)= 1.00000E-30   FLC( 14)= 1.00000E-30   FLC( 15)= 1.00000E-30
   FLC( 16)= 1.00000E-30   FLC( 17)= 1.00000E-30   FLC( 18)= 1.00000E-30   FLC( 19)= 1.00000E-30   FLC( 20)= 1.00000E-30
   FLC( 21)= 1.00000E-30   FLC( 22)= 1.00000E-30   FLC( 23)=-6.00000E+00   FLC( 24)=-4.00000E+00   FLC( 25)=-2.00000E+00
   FLC( 26)= 0.00000E+00   FLC( 27)= 2.00000E+00   FLC( 28)= 4.00000E+00   FLC( 29)= 8.00000E+00   FLC( 30)= 1.20000E+01
   FLC( 31)= 1.60000E+01   FLC( 32)= 2.00000E+01   FLC( 33)= 2.40000E+01   FLC( 34)= 1.00000E-30   FLC( 35)= 1.00000E-30
   FLC( 36)= 1.00000E-30   FLC( 37)= 1.00000E-30   FLC( 38)= 1.00000E-30   FLC( 39)= 1.00000E-30   FLC( 40)= 1.00000E-30
   FLC( 41)= 1.00000E-30   FLC( 42)= 1.00000E-30   FLC( 43)= 4.28000E+06   FLC( 44)= 1.00000E-30   FLC( 45)= 1.00000E-30
   FLC( 46)= 1.00000E-30   FLC( 47)= 1.00000E-30   FLC( 48)= 1.00000E-30   FLC( 49)= 1.00000E-30   FLC( 50)= 1.00000E-30
   FLC( 51)= 1.00000E-30   FLC( 52)= 1.00000E-30   FLC( 53)= 1.00000E-30   FLC( 54)= 1.00000E-30   FLC( 55)= 1.00000E-30
   FLC( 56)= 1.00000E-30   FLC( 57)= 1.00000E-30   FLC( 58)= 1.00000E-30   FLC( 59)= 1.00000E-30   FLC( 60)= 1.00000E-30
   FLC( 61)= 1.00000E-30   FLC( 62)= 1.00000E-30   FLC( 63)= 1.00000E-30   FLC( 64)= 1.00000E-30   FLC( 65)= 1.00000E-30
   FLC( 66)= 1.00000E-30   FLC( 67)= 1.00000E-30   FLC( 68)= 1.00000E-30   FLC( 69)= 1.00000E-30   FLC( 70)= 1.00000E-30
   FLC( 71)= 1.00000E-30   FLC( 72)= 1.00000E-30   FLC( 73)= 1.00000E-30   FLC( 74)=-1.00000E-30   FLC( 75)= 1.00000E-30
   FLC( 76)= 1.00000E-30   FLC( 77)= 1.00000E-30   FLC( 78)= 1.00000E-30   FLC( 79)= 1.00000E-30   FLC( 80)= 1.00000E-30
   FLC( 81)= 1.00000E-30   FLC( 82)= 1.00000E-30   FLC( 83)= 1.00000E-30   FLC( 84)= 1.00000E-30   FLC( 85)= 1.00000E-30
   FLC( 86)= 1.00000E-30   FLC( 87)= 1.00000E-30   FLC( 88)= 1.00000E-30   FLC( 89)= 1.00000E-30   FLC( 90)= 1.00000E-30
   FLC( 91)= 1.00000E-30   FLC( 92)= 1.00000E-30   FLC( 93)= 1.00000E-30   FLC( 94)= 6.00000E-01   FLC( 95)= 1.40000E+00
   FLC( 96)= 0.00000E+00   FLC( 97)=-1.00000E-30   FLC( 98)= 1.00000E-30   FLC( 99)= 1.00000E-30   FLC(100)= 1.00000E-30
   FLC(101)= 1.00000E-30   FLC(102)= 1.00000E-30   FLC(103)= 1.00000E-30   FLC(104)= 1.00000E-30   FLC(105)= 1.00000E-30
   FLC(106)= 1.00000E-30   FLC(107)= 1.00000E-30   FLC(108)= 1.00000E-30   FLC(109)= 1.00000E-30   FLC(110)= 1.00000E-30
   FLC(111)= 1.00000E-30   FLC(112)= 1.00000E-30   FLC(113)= 1.00000E-30   FLC(114)= 1.00000E-30   FLC(115)= 1.00000E-30
   FLC(116)= 1.00000E-30   FLC(117)=-1.00000E-30   FLC(118)= 1.00000E-30   FLC(119)= 1.00000E-30   FLC(120)= 1.00000E-30
   FLC(121)= 1.00000E-30   FLC(122)= 1.00000E-30   FLC(123)= 1.00000E-30   FLC(124)= 1.00000E-30   FLC(125)= 1.00000E-30
   FLC(126)= 1.00000E-30   FLC(127)= 1.00000E-30   FLC(128)= 1.00000E-30   FLC(129)= 1.00000E-30   FLC(130)= 1.00000E-30
   FLC(131)= 1.00000E-30   FLC(132)= 1.00000E-30   FLC(133)= 1.00000E-30   FLC(134)= 1.00000E-30   FLC(135)= 1.00000E-30
   FLC(136)= 1.00000E-30   FLC(137)=-1.00000E-30   FLC(138)= 1.00000E-30   FLC(139)= 1.00000E-30   FLC(140)= 1.00000E-30
   FLC(141)= 1.00000E-30   FLC(142)= 1.00000E-30   FLC(143)= 1.00000E-30   FLC(144)= 1.00000E-30   FLC(145)= 1.00000E-30
   FLC(146)= 1.00000E-30   FLC(147)= 1.00000E-30   FLC(148)= 1.00000E-30   FLC(149)= 1.00000E-30   FLC(150)= 1.00000E-30
   FLC(151)= 1.00000E-30   FLC(152)= 1.00000E-30   FLC(153)= 1.00000E-30   FLC(154)= 1.00000E-30   FLC(155)= 1.00000E-30
   FLC(156)= 1.00000E-30   FLC(157)= 1.00000E-30   FLC(158)= 1.00000E-30   FLC(159)= 0.00000E+00   FLC(160)= 1.00000E+00
 
  OPTI(  1)= 8.85000E+00  OPTI(  2)= 2.48000E+00  OPTI(  3)= 1.60000E-04  OPTI(  4)= 4.28000E+00
 
  SYNA(  1)= 4.14000E+00  SYNA(  2)= 1.00000E-30  SYNA(  3)= 1.00000E-30  SYNA(  4)= 1.00000E-30  SYNA(  5)=-2.00000E-01
  SYNA(  6)= 1.00000E-30  SYNA(  7)= 1.00000E-30  SYNA(  8)= 1.00000E-30  SYNA(  9)= 1.00000E-30  SYNA( 10)= 1.40130E-45
  SYNA( 11)= 1.00000E-30  SYNA( 12)= 1.00000E-30  SYNA( 13)= 1.00000E+00  SYNA( 14)= 1.00000E-30  SYNA( 15)= 1.00000E-30
  SYNA( 16)= 1.00000E-30  SYNA( 17)= 1.00000E-30  SYNA( 18)= 1.00000E-30  SYNA( 19)= 1.00000E-30
 
  BDIN(  1)= 1.00000E+01  BDIN(  2)= 0.00000E+00  BDIN(  3)= 2.58000E-01  BDIN(  4)= 5.89000E-01  BDIN(  5)= 1.26000E+00
  BDIN(  6)= 2.26000E+00  BDIN(  7)= 2.59000E+00  BDIN(  8)= 2.93000E+00  BDIN(  9)= 3.59000E+00  BDIN( 10)= 4.57000E+00
  BDIN( 11)= 6.26000E+00  BDIN( 12)= 1.00000E-30  BDIN( 13)= 1.00000E-30  BDIN( 14)= 1.00000E-30  BDIN( 15)= 1.00000E-30
  BDIN( 16)= 1.00000E-30  BDIN( 17)= 1.00000E-30  BDIN( 18)= 1.00000E-30  BDIN( 19)= 1.00000E-30  BDIN( 20)= 1.00000E-30
  BDIN( 21)= 1.00000E-30  BDIN( 22)= 0.00000E+00  BDIN( 23)= 8.00000E-02  BDIN( 24)= 1.60000E-01  BDIN( 25)= 3.23000E-01
  BDIN( 26)= 7.51000E-01  BDIN( 27)= 8.83000E-01  BDIN( 28)= 9.39000E-01  BDIN( 29)= 1.03200E+00  BDIN( 30)= 1.03200E+00
  BDIN( 31)= 1.03200E+00  BDIN( 32)= 1.00000E-30  BDIN( 33)= 1.00000E-30  BDIN( 34)= 1.00000E-30  BDIN( 35)= 1.00000E-30
  BDIN( 36)= 1.00000E-30  BDIN( 37)= 1.00000E-30  BDIN( 38)= 1.00000E-30  BDIN( 39)= 1.00000E-30  BDIN( 40)= 1.00000E-30
  BDIN( 41)= 1.00000E-30  BDIN( 42)= 0.00000E+00  BDIN( 43)= 1.00000E+00  BDIN( 44)= 1.42000E+00  BDIN( 45)= 2.01000E+00
  BDIN( 46)= 3.08000E+00  BDIN( 47)= 3.34000E+00  BDIN( 48)= 3.44000E+00  BDIN( 49)= 3.61000E+00  BDIN( 50)= 3.61000E+00
  BDIN( 51)= 3.61000E+00  BDIN( 52)= 1.00000E-30  BDIN( 53)= 1.00000E-30  BDIN( 54)= 1.00000E-30  BDIN( 55)= 1.00000E-30
  BDIN( 56)= 1.00000E-30  BDIN( 57)= 1.00000E-30  BDIN( 58)= 1.00000E-30  BDIN( 59)= 1.00000E-30  BDIN( 60)= 1.00000E-30
  BDIN( 61)= 1.00000E-30  BDIN( 62)= 0.00000E+00  BDIN( 63)= 1.86000E-01  BDIN( 64)= 2.86000E-01  BDIN( 65)= 4.24000E-01
  BDIN( 66)= 5.33000E-01  BDIN( 67)= 5.33000E-01  BDIN( 68)= 5.33000E-01  BDIN( 69)= 5.33000E-01  BDIN( 70)= 5.33000E-01
  BDIN( 71)= 5.33000E-01  BDIN( 72)= 1.00000E-30  BDIN( 73)= 1.00000E-30  BDIN( 74)= 1.00000E-30  BDIN( 75)= 1.00000E-30
  BDIN( 76)= 1.00000E-30  BDIN( 77)= 1.00000E-30  BDIN( 78)= 1.00000E-30  BDIN( 79)= 1.00000E-30  BDIN( 80)= 1.00000E-30
  BDIN( 81)= 1.00000E-30  BDIN( 82)= 1.00000E-30  BDIN( 83)= 1.00000E-30  BDIN( 84)= 1.00000E-30  BDIN( 85)= 1.00000E-30
  BDIN( 86)= 1.00000E-30  BDIN( 87)= 1.00000E-30  BDIN( 88)= 1.00000E-30  BDIN( 89)= 1.00000E-30  BDIN( 90)= 1.00000E-30
  BDIN( 91)= 1.00000E-30  BDIN( 92)= 1.00000E-30  BDIN( 93)= 1.00000E-30  BDIN( 94)= 1.00000E-30  BDIN( 95)= 1.00000E-30
  BDIN( 96)= 1.00000E-30  BDIN( 97)= 1.00000E-30  BDIN( 98)= 1.00000E-30  BDIN( 99)= 1.00000E-30  BDIN(100)= 1.00000E-30
  BDIN(101)= 1.00000E-30  BDIN(102)= 1.00000E-30  BDIN(103)= 1.00000E-30  BDIN(104)= 1.00000E-30  BDIN(105)= 1.00000E-30
  BDIN(106)= 1.00000E-30  BDIN(107)= 1.00000E-30  BDIN(108)= 1.00000E-30  BDIN(109)= 1.00000E-30  BDIN(110)= 1.00000E-30
  BDIN(111)= 1.00000E-30  BDIN(112)= 1.00000E-30  BDIN(113)= 1.00000E-30  BDIN(114)= 1.00000E-30  BDIN(115)= 1.00000E-30
  BDIN(116)= 1.00000E-30  BDIN(117)= 1.00000E-30  BDIN(118)= 1.00000E-30  BDIN(119)= 1.00000E-30  BDIN(120)= 1.00000E-30
  BDIN(121)= 1.00000E-30  BDIN(122)= 1.00000E+00  BDIN(123)= 1.00000E-30  BDIN(124)= 2.59000E+00  BDIN(125)= 3.67000E+00
  BDIN(126)= 1.00000E-30  BDIN(127)= 2.00000E+00  BDIN(128)= 1.00000E+00  BDIN(129)= 1.00000E+00
0**** FOLLOWING ARE THE IOM DATA BLOCKS ****
 
  BODY(  1)= 2.29591E-02  BODY(  2)= 2.17639E-02  BODY(  3)= 2.10455E-02  BODY(  4)= 2.08059E-02  BODY(  5)= 2.10455E-02
  BODY(  6)= 2.17639E-02  BODY(  7)= 2.46284E-02  BODY(  8)= 2.93715E-02  BODY(  9)= 3.59470E-02  BODY( 10)= 4.42904E-02
  BODY( 11)= 5.43198E-02  BODY( 12)= 1.00000E-30  BODY( 13)= 1.00000E-30  BODY( 14)= 1.00000E-30  BODY( 15)= 1.00000E-30
  BODY( 16)= 1.00000E-30  BODY( 17)= 1.00000E-30  BODY( 18)= 1.00000E-30  BODY( 19)= 1.00000E-30  BODY( 20)= 1.00000E-30
  BODY( 21)=-2.05992E-02  BODY( 22)=-1.37328E-02  BODY( 23)=-6.86641E-03  BODY( 24)= 0.00000E+00  BODY( 25)= 6.86641E-03
  BODY( 26)= 1.37328E-02  BODY( 27)= 2.74656E-02  BODY( 28)= 4.11985E-02  BODY( 29)= 5.49313E-02  BODY( 30)= 6.86641E-02
  BODY( 31)= 8.23969E-02  BODY( 32)= 1.00000E-30  BODY( 33)= 1.00000E-30  BODY( 34)= 1.00000E-30  BODY( 35)= 1.00000E-30
  BODY( 36)= 1.00000E-30  BODY( 37)= 1.00000E-30  BODY( 38)= 1.00000E-30  BODY( 39)= 1.00000E-30  BODY( 40)= 1.00000E-30
  BODY( 41)=-2.04910E-02  BODY( 42)=-1.36607E-02  BODY( 43)=-6.83034E-03  BODY( 44)= 0.00000E+00  BODY( 45)= 6.83034E-03
  BODY( 46)= 1.36607E-02  BODY( 47)= 2.73214E-02  BODY( 48)= 4.09820E-02  BODY( 49)= 5.46427E-02  BODY( 50)= 6.83034E-02
  BODY( 51)= 8.19641E-02  BODY( 52)= 1.00000E-30  BODY( 53)= 1.00000E-30  BODY( 54)= 1.00000E-30  BODY( 55)= 1.00000E-30
  BODY( 56)= 1.00000E-30  BODY( 57)= 1.00000E-30  BODY( 58)= 1.00000E-30  BODY( 59)= 1.00000E-30  BODY( 60)= 1.00000E-30
  BODY( 61)=-2.28863E-02  BODY( 62)=-1.52175E-02  BODY( 63)=-7.59671E-03  BODY( 64)= 0.00000E+00  BODY( 65)= 7.59671E-03
  BODY( 66)= 1.52175E-02  BODY( 67)= 3.06260E-02  BODY( 68)= 4.64049E-02  BODY( 69)= 6.27117E-02  BODY( 70)= 7.96714E-02
  BODY( 71)= 9.73672E-02  BODY( 72)= 1.00000E-30  BODY( 73)= 1.00000E-30  BODY( 74)= 1.00000E-30  BODY( 75)= 1.00000E-30
  BODY( 76)= 1.00000E-30  BODY( 77)= 1.00000E-30  BODY( 78)= 1.00000E-30  BODY( 79)= 1.00000E-30  BODY( 80)= 1.00000E-30
  BODY( 81)= 2.06801E-02  BODY( 82)= 2.07529E-02  BODY( 83)= 2.07931E-02  BODY( 84)= 2.08059E-02  BODY( 85)= 2.07931E-02
  BODY( 86)= 2.07529E-02  BODY( 87)= 2.05662E-02  BODY( 88)= 2.01641E-02  BODY( 89)= 1.94134E-02  BODY( 90)= 1.81349E-02
  BODY( 91)= 1.61097E-02  BODY( 92)= 1.00000E-30  BODY( 93)= 1.00000E-30  BODY( 94)= 1.00000E-30  BODY( 95)= 1.00000E-30
  BODY( 96)= 1.00000E-30  BODY( 97)= 1.00000E-30  BODY( 98)= 1.00000E-30  BODY( 99)= 1.00000E-30  BODY(100)= 1.00000E-30
  BODY(101)= 3.43321E-03  BODY(102)= 3.43321E-03  BODY(103)= 3.43321E-03  BODY(104)= 3.43321E-03  BODY(105)= 3.43321E-03
  BODY(106)= 3.43320E-03  BODY(107)= 3.43321E-03  BODY(108)= 3.43321E-03  BODY(109)= 3.43321E-03  BODY(110)= 3.43321E-03
  BODY(111)= 3.43321E-03  BODY(112)= 1.00000E-30  BODY(113)= 1.00000E-30  BODY(114)= 1.00000E-30  BODY(115)= 1.00000E-30
  BODY(116)= 1.00000E-30  BODY(117)= 1.00000E-30  BODY(118)= 1.00000E-30  BODY(119)= 1.00000E-30  BODY(120)= 1.00000E-30
  BODY(121)= 3.41517E-03  BODY(122)= 3.41517E-03  BODY(123)= 3.41517E-03  BODY(124)= 3.41517E-03  BODY(125)= 3.41517E-03
  BODY(126)= 3.41517E-03  BODY(127)= 3.41517E-03  BODY(128)= 3.41517E-03  BODY(129)= 3.41517E-03  BODY(130)= 3.41517E-03
  BODY(131)= 3.41517E-03  BODY(132)= 1.00000E-30  BODY(133)= 1.00000E-30  BODY(134)= 1.00000E-30  BODY(135)= 1.00000E-30
  BODY(136)= 1.00000E-30  BODY(137)= 1.00000E-30  BODY(138)= 1.00000E-30  BODY(139)= 1.00000E-30  BODY(140)= 1.00000E-30
  BODY(141)=-3.43321E-03  BODY(142)=-3.43321E-03  BODY(143)=-3.43321E-03  BODY(144)=-3.43321E-03  BODY(145)=-3.43321E-03
  BODY(146)=-3.43320E-03  BODY(147)=-3.43321E-03  BODY(148)=-3.43321E-03  BODY(149)=-3.43321E-03  BODY(150)=-3.43321E-03
  BODY(151)=-3.43321E-03  BODY(152)= 1.00000E-30  BODY(153)= 1.00000E-30  BODY(154)= 1.00000E-30  BODY(155)= 1.00000E-30
  BODY(156)= 1.00000E-30  BODY(157)= 1.00000E-30  BODY(158)= 1.00000E-30  BODY(159)= 1.00000E-30  BODY(160)= 1.00000E-30
  BODY(161)=-1.97888E-03  BODY(162)=-1.97888E-03  BODY(163)=-1.97888E-03  BODY(164)=-1.97888E-03  BODY(165)=-1.97888E-03
  BODY(166)=-1.97888E-03  BODY(167)=-1.97888E-03  BODY(168)=-1.97888E-03  BODY(169)=-1.97888E-03  BODY(170)=-1.97889E-03
  BODY(171)=-1.97889E-03  BODY(172)= 1.00000E-30  BODY(173)= 1.00000E-30  BODY(174)= 1.00000E-30  BODY(175)= 1.00000E-30
  BODY(176)= 1.00000E-30  BODY(177)= 1.00000E-30  BODY(178)= 1.00000E-30  BODY(179)= 1.00000E-30  BODY(180)= 1.00000E-30
  BODY(181)= 0.00000E+00  BODY(182)= 0.00000E+00  BODY(183)= 0.00000E+00  BODY(184)= 0.00000E+00  BODY(185)= 0.00000E+00
  BODY(186)= 0.00000E+00  BODY(187)= 0.00000E+00  BODY(188)= 0.00000E+00  BODY(189)= 0.00000E+00  BODY(190)= 0.00000E+00
  BODY(191)= 0.00000E+00  BODY(192)= 1.00000E-30  BODY(193)= 1.00000E-30  BODY(194)= 1.00000E-30  BODY(195)= 1.00000E-30
  BODY(196)= 1.00000E-30  BODY(197)= 1.00000E-30  BODY(198)= 1.00000E-30  BODY(199)= 1.00000E-30  BODY(200)= 1.00000E-30
  BODY(201)= 1.00000E-30  BODY(202)= 1.00000E-30  BODY(203)= 1.00000E-30  BODY(204)= 1.00000E-30  BODY(205)= 1.00000E-30
  BODY(206)= 1.00000E-30  BODY(207)= 1.00000E-30  BODY(208)= 1.00000E-30  BODY(209)= 1.00000E-30  BODY(210)= 1.00000E-30
  BODY(211)= 1.00000E-30  BODY(212)= 1.00000E-30  BODY(213)= 1.00000E-30  BODY(214)= 1.00000E-30  BODY(215)= 1.00000E-30
  BODY(216)= 1.00000E-30  BODY(217)= 1.00000E-30  BODY(218)= 1.00000E-30  BODY(219)= 1.00000E-30  BODY(220)= 1.00000E-30
  BODY(221)= 1.00000E-30  BODY(222)= 1.00000E-30  BODY(223)= 1.00000E-30  BODY(224)= 1.00000E-30  BODY(225)= 1.00000E-30
  BODY(226)= 1.00000E-30  BODY(227)= 1.00000E-30  BODY(228)= 1.00000E-30  BODY(229)= 1.00000E-30  BODY(230)= 1.00000E-30
  BODY(231)= 1.00000E-30  BODY(232)= 1.00000E-30  BODY(233)= 1.00000E-30  BODY(234)= 1.00000E-30  BODY(235)= 1.00000E-30
  BODY(236)= 1.00000E-30  BODY(237)= 1.00000E-30  BODY(238)= 1.00000E-30  BODY(239)= 1.00000E-30  BODY(240)= 1.00000E-30
  BODY(241)= 1.00000E-30  BODY(242)= 1.00000E-30  BODY(243)= 1.00000E-30  BODY(244)= 1.00000E-30  BODY(245)= 1.00000E-30
  BODY(246)= 1.00000E-30  BODY(247)= 1.00000E-30  BODY(248)= 1.00000E-30  BODY(249)= 1.00000E-30  BODY(250)= 1.00000E-30
  BODY(251)= 1.00000E-30  BODY(252)= 1.00000E-30  BODY(253)= 1.00000E-30  BODY(254)= 1.00000E-30  BODY(255)= 1.00000E-30
  BODY(256)= 1.00000E-30  BODY(257)= 1.00000E-30  BODY(258)= 1.00000E-30  BODY(259)= 1.00000E-30  BODY(260)= 1.00000E-30
  BODY(261)= 1.00000E-30  BODY(262)= 1.00000E-30  BODY(263)= 1.00000E-30  BODY(264)= 1.00000E-30  BODY(265)= 1.00000E-30
  BODY(266)= 1.00000E-30  BODY(267)= 1.00000E-30  BODY(268)= 1.00000E-30  BODY(269)= 1.00000E-30  BODY(270)= 1.00000E-30
  BODY(271)= 1.00000E-30  BODY(272)= 1.00000E-30  BODY(273)= 1.00000E-30  BODY(274)= 1.00000E-30  BODY(275)= 1.00000E-30
  BODY(276)= 1.00000E-30  BODY(277)= 1.00000E-30  BODY(278)= 1.00000E-30  BODY(279)= 1.00000E-30  BODY(280)= 1.00000E-30
  BODY(281)= 1.00000E-30  BODY(282)= 1.00000E-30  BODY(283)= 1.00000E-30  BODY(284)= 1.00000E-30  BODY(285)= 1.00000E-30
  BODY(286)= 1.00000E-30  BODY(287)= 1.00000E-30  BODY(288)= 1.00000E-30  BODY(289)= 1.00000E-30  BODY(290)= 1.00000E-30
  BODY(291)= 1.00000E-30  BODY(292)= 1.00000E-30  BODY(293)= 1.00000E-30  BODY(294)= 1.00000E-30  BODY(295)= 1.00000E-30
  BODY(296)= 1.00000E-30  BODY(297)= 1.00000E-30  BODY(298)= 1.00000E-30  BODY(299)= 1.00000E-30  BODY(300)= 1.00000E-30
  BODY(301)= 1.00000E-30  BODY(302)= 1.00000E-30  BODY(303)= 1.00000E-30  BODY(304)= 1.00000E-30  BODY(305)= 1.00000E-30
  BODY(306)= 1.00000E-30  BODY(307)= 1.00000E-30  BODY(308)= 1.00000E-30  BODY(309)= 1.00000E-30  BODY(310)= 1.00000E-30
  BODY(311)= 1.00000E-30  BODY(312)= 1.00000E-30  BODY(313)= 1.00000E-30  BODY(314)= 1.00000E-30  BODY(315)= 1.00000E-30
  BODY(316)= 1.00000E-30  BODY(317)= 1.00000E-30  BODY(318)= 1.00000E-30  BODY(319)= 1.00000E-30  BODY(320)= 1.00000E-30
  BODY(321)= 1.00000E-30  BODY(322)= 1.00000E-30  BODY(323)= 1.00000E-30  BODY(324)= 1.00000E-30  BODY(325)= 1.00000E-30
  BODY(326)= 1.00000E-30  BODY(327)= 1.00000E-30  BODY(328)= 1.00000E-30  BODY(329)= 1.00000E-30  BODY(330)= 1.00000E-30
  BODY(331)= 1.00000E-30  BODY(332)= 1.00000E-30  BODY(333)= 1.00000E-30  BODY(334)= 1.00000E-30  BODY(335)= 1.00000E-30
  BODY(336)= 1.00000E-30  BODY(337)= 1.00000E-30  BODY(338)= 1.00000E-30  BODY(339)= 1.00000E-30  BODY(340)= 1.00000E-30
  BODY(341)= 1.00000E-30  BODY(342)= 1.00000E-30  BODY(343)= 1.00000E-30  BODY(344)= 1.00000E-30  BODY(345)= 1.00000E-30
  BODY(346)= 1.00000E-30  BODY(347)= 1.00000E-30  BODY(348)= 1.00000E-30  BODY(349)= 1.00000E-30  BODY(350)= 1.00000E-30
  BODY(351)= 1.00000E-30  BODY(352)= 1.00000E-30  BODY(353)= 1.00000E-30  BODY(354)= 1.00000E-30  BODY(355)= 1.00000E-30
  BODY(356)= 1.00000E-30  BODY(357)= 1.00000E-30  BODY(358)= 1.00000E-30  BODY(359)= 1.00000E-30  BODY(360)= 1.00000E-30
  BODY(361)= 1.00000E-30  BODY(362)= 1.00000E-30  BODY(363)= 1.00000E-30  BODY(364)= 1.00000E-30  BODY(365)= 1.00000E-30
  BODY(366)= 1.00000E-30  BODY(367)= 1.00000E-30  BODY(368)= 1.00000E-30  BODY(369)= 1.00000E-30  BODY(370)= 1.00000E-30
  BODY(371)= 1.00000E-30  BODY(372)= 1.00000E-30  BODY(373)= 1.00000E-30  BODY(374)= 1.00000E-30  BODY(375)= 1.00000E-30
  BODY(376)= 1.00000E-30  BODY(377)= 1.00000E-30  BODY(378)= 1.00000E-30  BODY(379)= 1.00000E-30  BODY(380)= 1.00000E-30
  BODY(381)= 1.00000E-30  BODY(382)= 1.00000E-30  BODY(383)= 1.00000E-30  BODY(384)= 1.00000E-30  BODY(385)= 1.00000E-30
  BODY(386)= 1.00000E-30  BODY(387)= 1.00000E-30  BODY(388)= 1.00000E-30  BODY(389)= 1.00000E-30  BODY(390)= 1.00000E-30
  BODY(391)= 1.00000E-30  BODY(392)= 1.00000E-30  BODY(393)= 1.00000E-30  BODY(394)= 1.00000E-30  BODY(395)= 1.00000E-30
  BODY(396)= 1.00000E-30  BODY(397)= 1.00000E-30  BODY(398)= 1.00000E-30  BODY(399)= 1.00000E-30  BODY(400)= 1.00000E-30
1                               AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
                                         CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
                                                   DATCOM BODY ALONE CONFIGURATION
                                 APPROXIMATE AXISYMMETRIC BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 1
 
 -----------------------  FLIGHT CONDITIONS  ------------------------           --------------  REFERENCE DIMENSIONS  ------------
  MACH    ALTITUDE   VELOCITY    PRESSURE    TEMPERATURE     REYNOLDS             REF.      REFERENCE LENGTH   MOMENT REF. CENTER
 NUMBER                                                       NUMBER              AREA       LONG.     LAT.     HORIZ      VERT
             FT       FT/SEC     LB/FT**2       DEG R         1/FT               FT**2        FT        FT        FT        FT
0 0.600                                                    4.2800E+06             8.850      2.480     4.280     4.140    -0.200
0                                                               -------------------DERIVATIVE (PER DEGREE)-------------------
0 ALPHA     CD       CL       CM       CN       CA       XCP        CLA          CMA          CYB          CNB          CLB
0
   -6.0    0.023   -0.021   -0.0205  -0.023    0.021    0.895    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
   -4.0    0.022   -0.014   -0.0137  -0.015    0.021    0.898    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
   -2.0    0.021   -0.007   -0.0068  -0.008    0.021    0.899    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
    0.0    0.021    0.000    0.0000   0.000    0.021   ******    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
    2.0    0.021    0.007    0.0068   0.008    0.021    0.899    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
    4.0    0.022    0.014    0.0137   0.015    0.021    0.898    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
    8.0    0.025    0.027    0.0273   0.031    0.021    0.892    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
   12.0    0.029    0.041    0.0410   0.046    0.020    0.883    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
   16.0    0.036    0.055    0.0546   0.063    0.019    0.871    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
   20.0    0.044    0.069    0.0683   0.080    0.018    0.857    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
   24.0    0.054    0.082    0.0820   0.097    0.016    0.842    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
1          THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
  $BODY ZU(1) = -.595,-.476,-.372,-.138,.200,.334,.343,.343,.343,.343,           
        ZL(1) = -.595,-.715,-.754,-.805,-.868,-.868,-.868,-.868,-.868,-.868,     
  $END                                                                           
 CASEID ASYMMETRIC (CAMBERED) BODY SOLUTION,EXAMPLE PROBLEM 1,CASE 2             
 SAVE                                                                            
 NEXT CASE                                                                       
0 INPUT DIMENSIONS ARE IN FT, SCALE FACTOR IS 1.0000

1                               AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
                                         CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
                                                   DATCOM BODY ALONE CONFIGURATION
                                   ASYMMETRIC (CAMBERED) BODY SOLUTION,EXAMPLE PROBLEM 1,CASE 2
 
 -----------------------  FLIGHT CONDITIONS  ------------------------           --------------  REFERENCE DIMENSIONS  ------------
  MACH    ALTITUDE   VELOCITY    PRESSURE    TEMPERATURE     REYNOLDS             REF.      REFERENCE LENGTH   MOMENT REF. CENTER
 NUMBER                                                       NUMBER              AREA       LONG.     LAT.     HORIZ      VERT
             FT       FT/SEC     LB/FT**2       DEG R         1/FT               FT**2        FT        FT        FT        FT
0 0.600                                                    4.2800E+06             8.850      2.480     4.280     4.140    -0.200
0                                                               -------------------DERIVATIVE (PER DEGREE)-------------------
0 ALPHA     CD       CL       CM       CN       CA       XCP        CLA          CMA          CYB          CNB          CLB
0
   -6.0    0.022   -0.012   -0.0237  -0.014    0.021    1.638    3.227E-03    4.077E-03   -3.227E-03   -2.363E-03    0.000E+00
   -4.0    0.021   -0.007   -0.0156  -0.008    0.021    1.935    2.837E-03    4.059E-03   -2.837E-03   -2.352E-03    0.000E+00
   -2.0    0.021   -0.001   -0.0074  -0.002    0.021    4.616    2.859E-03    4.073E-03   -2.859E-03   -2.360E-03    0.000E+00
    0.0    0.021    0.005    0.0007   0.005    0.021    0.145    2.853E-03    4.069E-03   -2.853E-03   -2.357E-03    0.000E+00
    2.0    0.021    0.011    0.0088   0.011    0.021    0.783    2.818E-03    4.044E-03   -2.818E-03   -2.343E-03    0.000E+00
    4.0    0.022    0.016    0.0169   0.018    0.021    0.957    2.751E-03    3.996E-03   -2.751E-03   -2.315E-03    0.000E+00
    8.0    0.026    0.027    0.0326   0.030    0.022    1.084    2.537E-03    3.843E-03   -2.537E-03   -2.227E-03    0.000E+00
   12.0    0.031    0.036    0.0476   0.042    0.022    1.135    2.233E-03    3.622E-03   -2.233E-03   -2.098E-03    0.000E+00
   16.0    0.037    0.045    0.0616   0.053    0.023    1.161    3.100E-03    3.701E-03   -3.100E-03   -2.144E-03    0.000E+00
   20.0    0.048    0.061    0.0772   0.074    0.024    1.045    6.089E-03    4.404E-03   -6.089E-03   -2.552E-03    0.000E+00
   24.0    0.070    0.093    0.0968   0.114    0.026    0.852    9.984E-03    5.396E-03   -9.984E-03   -3.127E-03    0.000E+00
1          THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
  $FLTCON                                                                        
   NMACH = 3.0,                                                                  
   MACH(1) = 0.9,1.4,2.5,                                                        
   RNNUB = 6.4E6,9.96E6,17.0E6,                                                  
  $END                                                                           
 SAVE                                                                            
 CASEID ASYMMETRIC (CAMBERED) BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 3           
 NEXT CASE                                                                       
0 INPUT DIMENSIONS ARE IN FT, SCALE FACTOR IS 1.0000

1                               AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
                                         CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
                                                   DATCOM BODY ALONE CONFIGURATION
                                  ASYMMETRIC (CAMBERED) BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 3
 
 -----------------------  FLIGHT CONDITIONS  ------------------------           --------------  REFERENCE DIMENSIONS  ------------
  MACH    ALTITUDE   VELOCITY    PRESSURE    TEMPERATURE     REYNOLDS             REF.      REFERENCE LENGTH   MOMENT REF. CENTER
 NUMBER                                                       NUMBER              AREA       LONG.     LAT.     HORIZ      VERT
             FT       FT/SEC     LB/FT**2       DEG R         1/FT               FT**2        FT        FT        FT        FT
0 0.900                                                    6.4000E+06             8.850      2.480     4.280     4.140    -0.200
0                                                               -------------------DERIVATIVE (PER DEGREE)-------------------
0 ALPHA     CD       CL       CM       CN       CA       XCP        CLA          CMA          CYB          CNB          CLB
0
   -6.0    NDM      NDM       NDM     NDM      NDM      0.995    3.433E-03    3.415E-03   -3.433E-03   -1.979E-03    0.000E+00
   -4.0    NDM                                                                                                       0.000E+00
   -2.0    NDM                                                                                                       0.000E+00
    0.0    NDM                                                                                                       0.000E+00
    2.0    NDM                                                                                                       0.000E+00
    4.0    NDM                                                                                                       0.000E+00
    8.0    NDM                                                                                                       0.000E+00
   12.0    NDM                                                                                                       0.000E+00
   16.0    NDM                                                                                                       0.000E+00
   20.0    NDM                                                                                                       0.000E+00
   24.0    NDM                                                                                                       0.000E+00
0*** NDM PRINTED WHEN NO DATCOM METHODS EXIST
1                             AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
                                             CONFIGURATION AUXILIARY AND PARTIAL OUTPUT
                                                   DATCOM BODY ALONE CONFIGURATION
                                  ASYMMETRIC (CAMBERED) BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 3
 -----------------------  FLIGHT CONDITIONS  ------------------------           --------------  REFERENCE DIMENSIONS  ------------
  MACH    ALTITUDE   VELOCITY    PRESSURE    TEMPERATURE     REYNOLDS             REF.      REFERENCE LENGTH   MOMENT REF. CENTER
 NUMBER                                                       NUMBER              AREA       LONG.     LAT.     HORIZ      VERT
             FT       FT/SEC     LB/FT**2       DEG R         1/FT               FT**2        FT        FT        FT        FT
0 0.900                                                    6.4000E+06             8.850      2.480     4.280     4.140    -0.200


                                                       BASIC BODY PROPERTIES

            WETTED AREA      XCG     ZCG     BASE AREA     ZERO LIFT DRAG   BASE DRAG   FRICTION DRAG   PRESSURE DRAG
             0.1837E+02     4.14   -0.20       1.0320           NDM           NDM           NDM             NDM 
0*** NDM PRINTED WHEN NO DATCOM METHODS EXIST
1
1                               AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
                                         CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
                                                   DATCOM BODY ALONE CONFIGURATION
                                  ASYMMETRIC (CAMBERED) BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 3
 
 -----------------------  FLIGHT CONDITIONS  ------------------------           --------------  REFERENCE DIMENSIONS  ------------
  MACH    ALTITUDE   VELOCITY    PRESSURE    TEMPERATURE     REYNOLDS             REF.      REFERENCE LENGTH   MOMENT REF. CENTER
 NUMBER                                                       NUMBER              AREA       LONG.     LAT.     HORIZ      VERT
             FT       FT/SEC     LB/FT**2       DEG R         1/FT               FT**2        FT        FT        FT        FT
0 1.400                                                    9.9600E+06             8.850      2.480     4.280     4.140    -0.200
0                                                               -------------------DERIVATIVE (PER DEGREE)-------------------
0 ALPHA     CD       CL       CM       CN       CA       XCP        CLA          CMA          CYB          CNB          CLB
0
   -6.0    0.041   -0.034   -0.0260  -0.039    0.037    0.675    7.070E-03    4.588E-03   -7.070E-03   -2.658E-03    0.000E+00
   -4.0    0.039   -0.021   -0.0170  -0.024    0.037    0.712    6.202E-03    4.425E-03   -6.202E-03   -2.564E-03    0.000E+00
   -2.0    0.038   -0.010   -0.0083  -0.011    0.037    0.756    5.305E-03    4.249E-03   -5.305E-03   -2.462E-03    0.000E+00
    0.0    0.037    0.000    0.0000   0.000    0.037   ******    4.842E-03    4.156E-03   -4.842E-03   -2.408E-03    0.000E+00
    2.0    0.038    0.010    0.0083   0.011    0.037    0.756    5.305E-03    4.249E-03   -5.305E-03   -2.462E-03    0.000E+00
    4.0    0.039    0.021    0.0170   0.024    0.037    0.712    6.191E-03    4.420E-03   -6.191E-03   -2.561E-03    0.000E+00
    8.0    0.044    0.049    0.0353   0.055    0.037    0.642    7.795E-03    4.696E-03   -7.795E-03   -2.721E-03    0.000E+00
   12.0    0.054    0.084    0.0546   0.093    0.036    0.587    9.347E-03    4.933E-03   -9.347E-03   -2.858E-03    0.000E+00
   16.0    0.071    0.124    0.0748   0.139    0.034    0.538    1.110E-02    5.205E-03   -1.110E-02   -3.016E-03    0.000E+00
   20.0    0.098    0.172    0.0962   0.195    0.033    0.492    1.318E-02    5.569E-03   -1.318E-02   -3.227E-03    0.000E+00
   24.0    0.136    0.230    0.1193   0.265    0.031    0.450    1.542E-02    5.987E-03   -1.542E-02   -3.469E-03    0.000E+00
1                               AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
                                         CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
                                                   DATCOM BODY ALONE CONFIGURATION
                                  ASYMMETRIC (CAMBERED) BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 3
 
 -----------------------  FLIGHT CONDITIONS  ------------------------           --------------  REFERENCE DIMENSIONS  ------------
  MACH    ALTITUDE   VELOCITY    PRESSURE    TEMPERATURE     REYNOLDS             REF.      REFERENCE LENGTH   MOMENT REF. CENTER
 NUMBER                                                       NUMBER              AREA       LONG.     LAT.     HORIZ      VERT
             FT       FT/SEC     LB/FT**2       DEG R         1/FT               FT**2        FT        FT        FT        FT
0 2.500                                                    1.7000E+07             8.850      2.480     4.280     4.140    -0.200
0                                                               -------------------DERIVATIVE (PER DEGREE)-------------------
0 ALPHA     CD       CL       CM       CN       CA       XCP        CLA          CMA          CYB          CNB          CLB
0
   -6.0    0.027   -0.039   -0.0223  -0.041    0.023    0.537    7.792E-03    3.976E-03   -7.792E-03   -2.304E-03    0.000E+00
   -4.0    0.024   -0.024   -0.0145  -0.026    0.023    0.562    6.925E-03    3.803E-03   -6.925E-03   -2.204E-03    0.000E+00
   -2.0    0.023   -0.011   -0.0071  -0.012    0.023    0.590    6.032E-03    3.621E-03   -6.032E-03   -2.098E-03    0.000E+00
    0.0    0.023    0.000    0.0000   0.000    0.023   ******    5.572E-03    3.526E-03   -5.572E-03   -2.043E-03    0.000E+00
    2.0    0.023    0.011    0.0071   0.012    0.023    0.590    6.032E-03    3.621E-03   -6.032E-03   -2.098E-03    0.000E+00
    4.0    0.024    0.024    0.0145   0.026    0.023    0.562    6.943E-03    3.806E-03   -6.943E-03   -2.205E-03    0.000E+00
    8.0    0.030    0.056    0.0304   0.059    0.022    0.514    9.088E-03    4.233E-03   -9.088E-03   -2.453E-03    0.000E+00
   12.0    0.043    0.097    0.0484   0.104    0.022    0.467    1.231E-02    4.900E-03   -1.231E-02   -2.839E-03    0.000E+00
   16.0    0.066    0.154    0.0696   0.166    0.021    0.419    1.513E-02    5.504E-03   -1.513E-02   -3.189E-03    0.000E+00
   20.0    0.101    0.218    0.0924   0.239    0.020    0.386    1.524E-02    5.531E-03   -1.524E-02   -3.205E-03    0.000E+00
   24.0    0.144    0.276    0.1139   0.310    0.019    0.367    1.378E-02    5.211E-03   -1.378E-02   -3.019E-03    0.000E+00
1          THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
  $FLTCON                                                                        
   NMACH = 1.0,                                                                  
   MACH(1) = 2.5,                                                                
   RNNUB = 17.86E6,                                                              
   HYPERS = .TRUE.,                                                              
  $END                                                                           
  $BODY                                                                          
   DS = 0.0,                                                                     
  $END                                                                           
 CASEID HYPERSONIC BODY SOLUTION,  EXAMPLE PROBLEM 1, CASE 4                     
 NEXT CASE                                                                       
0 INPUT DIMENSIONS ARE IN FT, SCALE FACTOR IS 1.0000

1                               AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
                                         CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
                                                   DATCOM BODY ALONE CONFIGURATION
                                       HYPERSONIC BODY SOLUTION,  EXAMPLE PROBLEM 1, CASE 4
 
 -----------------------  FLIGHT CONDITIONS  ------------------------           --------------  REFERENCE DIMENSIONS  ------------
  MACH    ALTITUDE   VELOCITY    PRESSURE    TEMPERATURE     REYNOLDS             REF.      REFERENCE LENGTH   MOMENT REF. CENTER
 NUMBER                                                       NUMBER              AREA       LONG.     LAT.     HORIZ      VERT
             FT       FT/SEC     LB/FT**2       DEG R         1/FT               FT**2        FT        FT        FT        FT
0 2.500                                                    1.7860E+07             8.850      2.480     4.280     4.140    -0.200
0                                                               -------------------DERIVATIVE (PER DEGREE)-------------------
0 ALPHA     CD       CL       CM       CN       CA       XCP        CLA          CMA          CYB          CNB          CLB
0
   -6.0    0.016   -0.020   -0.0202  -0.022    0.014    0.915    4.413E-03    3.348E-03   -4.413E-03   -1.940E-03    0.000E+00
   -4.0    0.014   -0.012   -0.0135  -0.013    0.013    1.014    3.744E-03    3.351E-03   -3.744E-03   -1.942E-03    0.000E+00
   -2.0    0.013   -0.005   -0.0067  -0.006    0.013    1.135    3.075E-03    3.363E-03   -3.075E-03   -1.949E-03    0.000E+00
    0.0    0.013   -0.000   -0.0000  -0.000    0.013    0.625    2.741E-03    3.373E-03   -2.741E-03   -1.954E-03    0.000E+00
    2.0    0.013    0.005    0.0067   0.006    0.013    1.135    3.075E-03    3.363E-03   -3.075E-03   -1.949E-03    0.000E+00
    4.0    0.014    0.012    0.0135   0.013    0.013    1.014    3.736E-03    3.349E-03   -3.736E-03   -1.940E-03    0.000E+00
    8.0    0.019    0.030    0.0268   0.032    0.014    0.834    4.961E-03    3.319E-03   -4.961E-03   -1.923E-03    0.000E+00
   12.0    0.027    0.052    0.0400   0.056    0.016    0.708    6.037E-03    3.324E-03   -6.037E-03   -1.926E-03    0.000E+00
   16.0    0.041    0.078    0.0534   0.086    0.018    0.619    6.927E-03    3.400E-03   -6.927E-03   -1.970E-03    0.000E+00
   20.0    0.060    0.107    0.0672   0.121    0.020    0.553    7.539E-03    3.496E-03   -7.539E-03   -2.026E-03    0.000E+00
   24.0    0.086    0.138    0.0814   0.161    0.022    0.504    7.992E-03    3.593E-03   -7.992E-03   -2.082E-03    0.000E+00
1          THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
1 END OF JOB.
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