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****************************************************
* 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 *
****************************************************
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 ******************************
$FLTCON NMACH=4.0, MACH=0.6,0.9,1.4,2.5, LOOP=1.0, NALT=4.0,
ALT=0.0, 2000.0, 40000.0, 90000.0, HYPERS=.FALSE.,
NALPHA=11.0, ALSCHD=-6.0, -4.0, -2.0, 0.0, 2.0, 4.0,
8.0, 12.0, 16.0, 20.0, 24.0$
$OPTINS SREF=8.05, CBARR=2.46, BLREF=4.28$
$SYNTHS XW=3.61, ZW=-.98, ALIW=2.0,XCG=4.14$
$WGPLNF CHRDTP=0.64, SSPNE=1.59, SSPN=1.59,CHRDR=2.90, SAVSI=55.0, CHSTAT=0.0,
SWAFP=0.0, TWISTA=0.0, SSPNDD=0.0, DHDADI=0.0, DHDADO=0.0, TYPE=1.0$
$WGSCHR DELTAY=2.05, XOVC=0.4, CLI=0.127, ALPHAI=0.123, CLALPA=0.1335,
TOVC=0.11,
CLMAX(1)=1.195, CMO=-0.0262, LERI=0.0134, CAMBER=.TRUE., CLAMO=0.105,
TCEFF=0.055$
CASEID STRAIGHT TAPERED EXPOSED WING SOLUTION, EXAMPLE PROBLEM 2, CASE 1
SAVE
DUMP A
NEXT CASE
$FLTCON NMACH=2.0,MACH=0.6,2.5, LOOP=2.0, NALT=2.0, ALT=0.0, 90000.0$
$SYNTHS XW=2.497, ZW=0.710$
$WGPLNF SSPNOP=1.11, CHRDBP=2.24, CHRDR=4.01,
SAVSI=75.1, SAVSO=55.0, TYPE=3.0$
$WGSCHR TOVC=0.1, LERI=0.011, LERO=0.0138, TOVCO=0.12,
XOVCO=0.40, CMOT=-0.0262$
CASEID EXPOSED CRANKED WING SOLUTION, EXAMPLE PROBLEM 2, CASE 2
SAVE
NEXT CASE
$FLTCON LOOP=3.0$
$WGPLNF TYPE=2.0$
CASEID EXPOSED DOUBLE DELTA WING SOLUTION, EXAMPLE PROBLEM 2, CASE 3
NEXT CASE
1 THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
$FLTCON NMACH=4.0, MACH=0.6,0.9,1.4,2.5, LOOP=1.0, NALT=4.0,
ALT=0.0, 2000.0, 40000.0, 90000.0, HYPERS=.FALSE.,
NALPHA=11.0, ALSCHD=-6.0, -4.0, -2.0, 0.0, 2.0, 4.0,
8.0, 12.0, 16.0, 20.0, 24.0$
$OPTINS SREF=8.05, CBARR=2.46, BLREF=4.28$
$SYNTHS XW=3.61, ZW=-.98, ALIW=2.0,XCG=4.14$
$WGPLNF CHRDTP=0.64, SSPNE=1.59, SSPN=1.59,CHRDR=2.90, SAVSI=55.0, CHSTAT=0.0,
SWAFP=0.0, TWISTA=0.0, SSPNDD=0.0, DHDADI=0.0, DHDADO=0.0, TYPE=1.0$
$WGSCHR DELTAY=2.05, XOVC=0.4, CLI=0.127, ALPHAI=0.123, CLALPA=0.1335,
TOVC=0.11,
CLMAX(1)=1.195, CMO=-0.0262, LERI=0.0134, CAMBER=.TRUE., CLAMO=0.105,
TCEFF=0.055$
CASEID STRAIGHT TAPERED EXPOSED WING SOLUTION, EXAMPLE PROBLEM 2, CASE 1
SAVE
DUMP A
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
A( 1)= 5.62860E+00 A( 2)= 1.28000E-30 A( 3)= 5.62860E+00 A( 4)= 5.62860E+00 A( 5)= 1.79661E+00
A( 6)= 1.00000E+00 A( 7)= 1.79661E+00 A( 8)= 1.00000E-30 A( 9)= 1.00000E-30 A( 10)= 2.90000E+00
A( 11)= 1.00000E-30 A( 12)= 1.00000E-30 A( 13)= 1.00000E-30 A( 14)= 1.00000E-30 A( 15)= 2.01047E+00
A( 16)= 2.01047E+00 A( 17)= 6.40000E-01 A( 18)= 7.83019E-01 A( 19)= 1.00000E+00 A( 20)= 1.00000E-30
A( 21)= 1.59000E+00 A( 22)= 1.00000E-30 A( 23)= 1.59000E+00 A( 24)= 1.00000E-30 A( 25)= 2.20690E-01
A( 26)= 2.20690E-01 A( 27)= 2.20690E-01 A( 28)= 1.00000E+00 A( 29)= 2.91076E+00 A( 30)= 1.89900E+00
A( 31)= 6.25819E-01 A( 32)= 6.25819E-01 A( 33)= 1.59000E+00 A( 34)= 5.50000E+01 A( 35)= 9.59931E-01
A( 36)= 8.19152E-01 A( 37)= 5.73576E-01 A( 38)= 1.42815E+00 A( 39)= 9.59931E-01 A( 40)= 4.70116E+01
A( 41)= 8.20506E-01 A( 42)= 7.31491E-01 A( 43)= 6.81851E-01 A( 44)= 1.07280E+00 A( 45)= 8.20506E-01
A( 46)= 3.56578E+01 A( 47)= 6.22346E-01 A( 48)= 5.82943E-01 A( 49)= 8.12513E-01 A( 50)= 7.17456E-01
A( 51)= 6.22346E-01 A( 52)= 3.87566E-01 A( 53)= 6.76431E-03 A( 54)= 6.76426E-03 A( 55)= 9.99977E-01
A( 56)= 6.76441E-03 A( 57)= 6.76431E-03 A( 58)= 5.50000E+01 A( 59)= 9.59931E-01 A( 60)= 8.19152E-01
A( 61)= 5.73576E-01 A( 62)= 1.42815E+00 A( 63)= 9.59931E-01 A( 64)= 4.70116E+01 A( 65)= 8.20506E-01
A( 66)= 7.31491E-01 A( 67)= 6.81851E-01 A( 68)= 1.07280E+00 A( 69)= 8.20506E-01 A( 70)= 3.56578E+01
A( 71)= 6.22346E-01 A( 72)= 5.82943E-01 A( 73)= 8.12513E-01 A( 74)= 7.17456E-01 A( 75)= 6.22346E-01
A( 76)= 3.87566E-01 A( 77)= 6.76431E-03 A( 78)= 6.76426E-03 A( 79)= 9.99977E-01 A( 80)= 6.76441E-03
A( 81)= 6.76431E-03 A( 82)= 0.00000E+00 A( 83)= 0.00000E+00 A( 84)= 0.00000E+00 A( 85)= 1.00000E+00
A( 86)= 0.00000E+00 A( 87)= 0.00000E+00 A( 88)= 0.00000E+00 A( 89)= 0.00000E+00 A( 90)= 0.00000E+00
A( 91)= 1.00000E+00 A( 92)= 0.00000E+00 A( 93)= 0.00000E+00 A( 94)= 0.00000E+00 A( 95)= 0.00000E+00
A( 96)= 0.00000E+00 A( 97)= 1.00000E+00 A( 98)= 0.00000E+00 A( 99)= 0.00000E+00 A(100)= 0.00000E+00
A(101)= 0.00000E+00 A(102)= 0.00000E+00 A(103)= 1.00000E+00 A(104)= 0.00000E+00 A(105)= 0.00000E+00
A(106)= 5.50000E+01 A(107)= 9.59931E-01 A(108)= 8.19152E-01 A(109)= 5.73576E-01 A(110)= 1.42815E+00
A(111)= 9.59931E-01 A(112)= 0.00000E+00 A(113)= 0.00000E+00 A(114)= 0.00000E+00 A(115)= 1.00000E+00
A(116)= 0.00000E+00 A(117)= 0.00000E+00 A(118)= 2.20690E-01 A(119)= 5.62860E+00 A(120)= 1.79661E+00
A(121)= 2.01047E+00 A(122)= 2.01047E+00 A(123)= 4.75379E-01 A(124)= 8.46243E-01 A(125)= 4.13593E+00
A(126)=-1.08652E+00 A(127)= 2.85598E+01 A(128)= 3.50000E+00 A(129)= 4.24094E+06 A(130)= 6.25819E-01
A(131)= 1.33500E-01 A(132)= 1.19500E+00 A(133)= 0.00000E+00 A(134)=-8.28311E-01 A(135)= 1.00000E-30
A(136)= 6.25819E-01 A(137)= 1.00000E+00 A(138)= 0.00000E+00 A(139)= 0.00000E+00 A(140)= 0.00000E+00
A(141)= 1.00000E+00 A(142)= 0.00000E+00 A(143)= 0.00000E+00 A(144)= 8.60750E+00 A(145)= 8.45000E-01
A(146)= 1.00000E-30 A(147)= 2.63384E+01 A(148)= 4.59692E-01 A(149)= 4.43672E-01 A(150)= 8.96189E-01
A(151)= 4.95065E-01 A(152)= 4.59692E-01 A(153)= 2.68220E+01 A(154)= 4.68133E-01 A(155)= 4.51221E-01
A(156)= 8.92412E-01 A(157)= 5.05619E-01 A(158)= 4.68133E-01 A(159)= 5.82759E-01 A(160)= 4.06108E+00
A(161)= 1.39638E+00 A(162)= 1.00000E+00 A(163)= 1.79661E+00 A(164)= 7.95000E-01 A(165)= 7.95000E-01
A(166)= 1.00000E-30 A(167)= 1.00000E-30 A(168)= 1.00000E-30 A(169)= 1.00000E-30 A(170)= 1.82759E-01
A(171)= 1.00000E-30 A(172)= 1.00000E-30 A(173)= 5.30000E-01 A(174)= 4.00000E-01 A(175)= 4.06822E+01
A(176)= 7.10038E-01 A(177)= 6.51863E-01 A(178)= 7.58337E-01 A(179)= 8.59595E-01 A(180)= 7.10038E-01
A(181)= 0.00000E+00 A(182)= 0.00000E+00 A(183)= 0.00000E+00 A(184)= 1.00000E+00 A(185)= 0.00000E+00
A(186)= 0.00000E+00 A(187)= 4.06822E+01 A(188)= 7.10038E-01 A(189)= 6.51863E-01 A(190)= 7.58337E-01
A(191)= 8.59595E-01 A(192)= 7.10038E-01 A(193)= 1.00000E-30 A(194)= 1.00000E-30 A(195)= 8.93762E-01
1 AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
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