ex5.out

Digital DATCOM Source Code and Examples

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 OF THE POSSIBILITY OF SUCH DAMAGES.
  ****************************************************
  *    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 [phone],   FAX [phone]    *
  ****************************************************
 Preparing to start the big loop
 At 1000
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  ******************************

 DIM FT                                                                          
 PART                                                                            
  $FLTCON  NALPHA=9.0, ALSCHD(1)=-2.0,0.0,2.0,4.0,8.0,12.0,16.0,20.0,24.0$       
  $FLTCON  NMACH=1.0, MACH(1)=0.6, RNNUB(1)=4.26E6$                              
  $OPTINS SREF=2.25, CBARR=0.822, BLREF=3.00$                                    
  $SYNTHS XCG=2.60, ZCG=0.0, XW=1.70, ZW=0.0, ALIW=0.0$                          
  $BODY NX=10.0,BNOSE=2.0,BTAIL=1.0,BLN=1.46,BLA=1.97,                           
    X(1)=0.0, .175,.322,.530,.850,1.46,2.5,3.43,3.97,4.57,                       
    R(1)=0.0, .0417,.0833,.125,.1665,.208,.208,.208,.178,.138$                   
  $WGPLNF CHRDTP=0.346,SSPNE=1.29,SSPN=1.5,CHRDR=1.16,SAVSI=45.0,CHSTAT=0.25,    
   SWAFP=0.0,TWISTA=0.0,SSPNDD=0.0,DHDADI=0.0,DHDADO=0.0,TYPE=1.0$               
  $WGSCHR TOVC=.06,DELTAY=1.3,XOVC=0.4,CLI=0.0,ALPHAI=0.0,CLALPA(1)=0.131,       
   CLMAX(1)=.82,CMO=0.0,LERI=.0025,CLAMO=.105$                                   
  $WGSCHR  CLMAXL=0.8, TCEFF=.03$                                                
 CASEID BODY-WING DAMPING DERIVATIVES, EXAMPLE PROBLEM 5, CASE 1                 
 DAMP                                                                            
 SAVE                                                                            
 DUMP DYN                                                                        
 NEXT CASE                                                                       
  $SYMFLP NDELTA=6.0, DELTA(1)=0.,.10,.20,.30,.40,.60, PHETE=.0522,              
   CHRDFI=.2094, CHRDFO=.1554, SPANFI=0.208, SPANFO=.708, FTYPE=1.0,             
   CB=.01125, TC=.0225, PHETEP=.0391, NTYPE=1.0$                                 
 CASEID PLAIN FLAPS ON WING, EXAMPLE PROBLEM 5, CASE 2                           
 DUMP FCM                                                                        
 NEXT CASE                                                                       
1          THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
 DIM FT                                                                          
 PART                                                                            
  $FLTCON  NALPHA=9.0, ALSCHD(1)=-2.0,0.0,2.0,4.0,8.0,12.0,16.0,20.0,24.0$       
  $FLTCON  NMACH=1.0, MACH(1)=0.6, RNNUB(1)=4.26E6$                              
  $OPTINS SREF=2.25, CBARR=0.822, BLREF=3.00$                                    
  $SYNTHS XCG=2.60, ZCG=0.0, XW=1.70, ZW=0.0, ALIW=0.0$                          
  $BODY NX=10.0,BNOSE=2.0,BTAIL=1.0,BLN=1.46,BLA=1.97,                           
    X(1)=0.0, .175,.322,.530,.850,1.46,2.5,3.43,3.97,4.57,                       
    R(1)=0.0, .0417,.0833,.125,.1665,.208,.208,.208,.178,.138$                   
  $WGPLNF CHRDTP=0.346,SSPNE=1.29,SSPN=1.5,CHRDR=1.16,SAVSI=45.0,CHSTAT=0.25,    
   SWAFP=0.0,TWISTA=0.0,SSPNDD=0.0,DHDADI=0.0,DHDADO=0.0,TYPE=1.0$               
  $WGSCHR TOVC=.06,DELTAY=1.3,XOVC=0.4,CLI=0.0,ALPHAI=0.0,CLALPA(1)=0.131,       
   CLMAX(1)=.82,CMO=0.0,LERI=.0025,CLAMO=.105$                                   
  $WGSCHR  CLMAXL=0.8, TCEFF=.03$                                                
 CASEID BODY-WING DAMPING DERIVATIVES, EXAMPLE PROBLEM 5, CASE 1                 
 DAMP                                                                            
 SAVE                                                                            
 DUMP DYN                                                                        
 NEXT CASE                                                                       
0 INPUT DIMENSIONS ARE IN FT, SCALE FACTOR IS 1.0000

 Return to main program from M01O01
 Return to main program from M50O62
 Return to main program from M02O02
 Return to main program from M51O63
 WARNING*** BODY ALONE DYNAMIC DERIVATIVE METHOD VALID FOR NOSE CYLINDER ONLY
            TAIL EFFECTS IGNORED]
 
   DYN(  1)= 1.00000E-30   DYN(  2)=-1.37623E-02   DYN(  3)= 1.00000E-30   DYN(  4)= 1.00000E-30   DYN(  5)= 1.00000E-30
   DYN(  6)= 1.00000E-30   DYN(  7)= 1.00000E-30   DYN(  8)= 1.00000E-30   DYN(  9)= 1.00000E-30   DYN( 10)= 1.00000E-30
   DYN( 11)= 1.00000E-30   DYN( 12)= 1.00000E-30   DYN( 13)= 1.00000E-30   DYN( 14)= 1.00000E-30   DYN( 15)= 1.00000E-30
   DYN( 16)= 1.00000E-30   DYN( 17)= 1.00000E-30   DYN( 18)= 1.00000E-30   DYN( 19)= 1.00000E-30   DYN( 20)= 1.00000E-30
   DYN( 21)=-5.92921E-03   DYN( 22)= 1.00000E-30   DYN( 23)= 1.00000E-30   DYN( 24)= 1.00000E-30   DYN( 25)= 1.00000E-30
   DYN( 26)= 1.00000E-30   DYN( 27)= 1.00000E-30   DYN( 28)= 1.00000E-30   DYN( 29)= 1.00000E-30   DYN( 30)= 1.00000E-30
   DYN( 31)= 1.00000E-30   DYN( 32)= 1.00000E-30   DYN( 33)= 1.00000E-30   DYN( 34)= 1.00000E-30   DYN( 35)= 1.00000E-30
   DYN( 36)= 1.00000E-30   DYN( 37)= 1.00000E-30   DYN( 38)= 1.00000E-30   DYN( 39)= 1.00000E-30   DYN( 40)= 4.78802E-01
   DYN( 41)= 1.00000E-30   DYN( 42)= 1.00000E-30   DYN( 43)= 1.00000E-30   DYN( 44)= 0.00000E+00   DYN( 45)= 4.66432E-02
   DYN( 46)=-1.50367E-01   DYN( 47)= 4.66429E-02   DYN( 48)= 4.66432E-02   DYN( 49)= 4.67195E-02   DYN( 50)= 4.66050E-02
   DYN( 51)= 4.51856E-02   DYN( 52)= 3.82381E-02   DYN( 53)= 2.44164E-02   DYN( 54)= 7.06771E-03   DYN( 55)=-1.18053E-02
   DYN( 56)= 1.00000E-30   DYN( 57)= 1.00000E-30   DYN( 58)= 1.00000E-30   DYN( 59)= 1.00000E-30   DYN( 60)= 1.00000E-30
   DYN( 61)= 1.00000E-30   DYN( 62)= 1.00000E-30   DYN( 63)= 1.00000E-30   DYN( 64)= 1.00000E-30   DYN( 65)= 1.00000E-30
   DYN( 66)= 1.00000E-30   DYN( 67)= 0.00000E+00   DYN( 68)= 1.00000E+00   DYN( 69)=-3.86146E-02   DYN( 70)= 3.33513E+00
   DYN( 71)=-2.45063E-01   DYN( 72)=-1.13060E-03   DYN( 73)=-7.97236E-04   DYN( 74)=-1.13060E-03   DYN( 75)=-2.13507E-03
   DYN( 76)=-6.09190E-03   DYN( 77)=-1.23164E-02   DYN( 78)=-1.83899E-02   DYN( 79)=-2.19844E-02   DYN( 80)=-2.14480E-02
   DYN( 81)= 1.00000E-30   DYN( 82)= 1.00000E-30   DYN( 83)= 1.00000E-30   DYN( 84)= 1.00000E-30   DYN( 85)= 1.00000E-30
   DYN( 86)= 1.00000E-30   DYN( 87)= 1.00000E-30   DYN( 88)= 1.00000E-30   DYN( 89)= 1.00000E-30   DYN( 90)= 1.00000E-30
   DYN( 91)= 1.00000E-30   DYN( 92)=-1.55970E-01   DYN( 93)= 9.05538E-01   DYN( 94)= 6.40340E-03   DYN( 95)=-2.42433E-04
   DYN( 96)=-1.62232E-03   DYN( 97)= 1.00000E-30   DYN( 98)= 3.25393E-03   DYN( 99)= 6.50913E-03   DYN(100)= 1.28848E-02
   DYN(101)= 1.76882E-02   DYN(102)= 1.91888E-02   DYN(103)= 1.65058E-02   DYN(104)= 1.39972E-02   DYN(105)= 1.00000E-30
   DYN(106)= 1.00000E-30   DYN(107)= 1.00000E-30   DYN(108)= 1.00000E-30   DYN(109)= 1.00000E-30   DYN(110)= 1.00000E-30
   DYN(111)= 1.00000E-30   DYN(112)= 1.00000E-30   DYN(113)= 1.00000E-30   DYN(114)= 1.00000E-30   DYN(115)= 1.00000E-30
   DYN(116)=-1.02747E-03   DYN(117)= 1.00000E-30   DYN(118)= 2.06168E-03   DYN(119)= 4.09649E-03   DYN(120)= 7.84503E-03
   DYN(121)= 9.47595E-03   DYN(122)= 7.44952E-03   DYN(123)= 2.35638E-03   DYN(124)=-8.26683E-04   DYN(125)= 1.00000E-30
   DYN(126)= 1.00000E-30   DYN(127)= 1.00000E-30   DYN(128)= 1.00000E-30   DYN(129)= 1.00000E-30   DYN(130)= 1.00000E-30
   DYN(131)= 1.00000E-30   DYN(132)= 1.00000E-30   DYN(133)= 1.00000E-30   DYN(134)= 1.00000E-30   DYN(135)= 1.00000E-30
   DYN(136)=-3.44874E-04   DYN(137)= 1.00000E-30   DYN(138)= 6.92011E-04   DYN(139)= 1.37500E-03   DYN(140)= 2.63321E-03
   DYN(141)= 3.18064E-03   DYN(142)= 2.50046E-03   DYN(143)= 7.90930E-04   DYN(144)=-2.77479E-04   DYN(145)= 1.00000E-30
   DYN(146)= 1.00000E-30   DYN(147)= 1.00000E-30   DYN(148)= 1.00000E-30   DYN(149)= 1.00000E-30   DYN(150)= 1.00000E-30
   DYN(151)= 1.00000E-30   DYN(152)= 1.00000E-30   DYN(153)= 1.00000E-30   DYN(154)= 1.00000E-30   DYN(155)= 1.00000E-30
   DYN(156)= 4.65658E-01   DYN(157)= 1.00000E+00   DYN(158)= 4.65374E-01   DYN(159)= 4.69921E-01   DYN(160)= 4.91607E-01
   DYN(161)= 5.66067E-01   DYN(162)= 7.03442E-01   DYN(163)= 9.00384E-01   DYN(164)= 1.03847E+00   DYN(165)= 1.00000E-30
   DYN(166)= 1.00000E-30   DYN(167)= 1.00000E-30   DYN(168)= 1.00000E-30   DYN(169)= 1.00000E-30   DYN(170)= 1.00000E-30
   DYN(171)= 1.00000E-30   DYN(172)= 1.00000E-30   DYN(173)= 1.00000E-30   DYN(174)= 1.00000E-30   DYN(175)= 1.00000E-30
   DYN(176)=-2.92747E-01   DYN(177)= 0.00000E+00   DYN(178)= 4.84686E-01   DYN(179)= 2.01527E+00   DYN(180)= 5.64482E-01
   DYN(181)= 2.14793E+00   DYN(182)=-2.85684E-03   DYN(183)=-5.37371E-01   DYN(184)= 7.74307E-03   DYN(185)= 6.37788E-03
   DYN(186)= 7.74309E-03   DYN(187)= 1.18566E-02   DYN(188)= 2.80606E-02   DYN(189)= 5.35511E-02   DYN(190)= 7.84231E-02
   DYN(191)= 9.31435E-02   DYN(192)= 9.09467E-02   DYN(193)= 1.00000E-30   DYN(194)= 1.00000E-30   DYN(195)= 1.00000E-30
   DYN(196)= 1.00000E-30   DYN(197)= 1.00000E-30   DYN(198)= 1.00000E-30   DYN(199)= 1.00000E-30   DYN(200)= 1.00000E-30