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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
NDM 0.021 0.000 0.0000 0.000 0.021 0.900 3.433E-03 3.415E-03 -3.433E-03 -1.979E-03 0.000E+00
0*** NDM PRINTED WHEN NO DATCOM METHODS EXIST
Return to main program from M57O71
1 THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
$BODY ZU(1)= -.595,-.476,-.372,-.138, .200,.334,.343,.343,.343,.343,
ZL(1)= -.595, -.715, -.754, -.805, -.868, -.868, -.868, -.868, -.868$
CASEID ASYMMETRIC (CAMBERED) BODY SOLUTION, EXAMPLE PROBLEM 1, CASE 2
SAVE
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
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 0.025 -0.024 -0.0033 -0.026 0.022 0.126 3.227E-03 3.902E-03 -3.227E-03 -2.261E-03 0.000E+00
-4.0 0.023 -0.018 0.0042 -0.020 0.022 -0.211 2.727E-03 3.806E-03 -2.727E-03 -2.205E-03 0.000E+00
-2.0 0.022 -0.013 0.0119 -0.014 0.021 -0.871 2.799E-03 3.856E-03 -2.799E-03 -2.234E-03 0.000E+00
0.0 0.021 -0.007 0.0197 -0.007 0.021 -2.708 2.844E-03 3.886E-03 -2.844E-03 -2.252E-03 0.000E+00
2.0 0.021 -0.002 0.0274 -0.001 0.021 ****** 2.033E-03 3.669E-03 -2.033E-03 -2.126E-03 0.000E+00
4.0 0.021 0.004 0.0352 0.006 0.021 6.250 3.928E-03 4.136E-03 -3.928E-03 -2.397E-03 0.000E+00
8.0 0.023 0.024 0.0527 0.027 0.020 1.984 7.719E-03 5.069E-03 -7.719E-03 -2.937E-03 0.000E+00
12.0 0.032 0.062 0.0747 0.067 0.019 1.118 1.151E-02 6.003E-03 -1.151E-02 -3.478E-03 0.000E+00
16.0 0.051 0.116 0.1008 0.126 0.017 0.802 1.530E-02 6.936E-03 -1.530E-02 -4.019E-03 0.000E+00
20.0 0.082 0.185 0.1304 0.202 0.014 0.645 1.909E-02 7.869E-03 -1.909E-02 -4.560E-03 0.000E+00
NDM 0.021 -0.007 0.0197 -0.007 0.021 -2.708 1.373E-04 3.203E-03 -1.373E-04 -1.856E-03 0.000E+00
0*** NDM PRINTED WHEN NO DATCOM METHODS EXIST
Return to main program from M57O71
1 THE FOLLOWING IS A LIST OF ALL INPUT CARDS FOR THIS CASE.
0
$FLTCON NMACH=3.0, MACH(1)=0.9,1.4,2.5, RNNUB=6.4E6, 9.96E6, 17.0E6$
SAVE
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
1 AUTOMATED STABILITY AND CONTROL METHODS PER APRIL 1976 VERSION OF DATCOM
CHARACTERISTICS AT ANGLE OF ATTACK AND IN SIDESLIP
DATCOM BODY ALONE CONFIGURATION
----------------------- 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
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