Unknown
2001-01-01
$Revision: 1.12 $
Mk-82
This model was created using publicly available data, publicly available
technical reports, textbooks, and guesses. It contains no proprietary or
restricted data. If this model has been validated at all, it would be
only to the extent that it seems to "fly right", and that it possibly
complies with published, publicly known, performance data (maximum speed,
endurance, etc.). Or, it could be a gross approximation, with the only
similarity to an actual object being the name. Thus, this model is meant
for educational and entertainment purposes only.
This simulation model is not endorsed by the manufacturer. This model is not
to be sold.
2.54
0.9
0.9
0
0
0
0
33.08
0
0
0
0
0
31
0
0
0.66
633
633
500
31
0
0
0
0
0
0
0
0
10000
200000
0.0
NONE
0
66
0
0
0
0
0
10000
200000
0.0
NONE
0
Drag_minimum
aero/qbar-psf
metrics/Sw-sqft
velocities/mach
0.2000 0.1400
0.4000 0.1390
0.8000 0.1440
0.9000 0.1490
0.9500 0.2110
0.9800 0.2520
1.0000 0.2810
1.0200 0.3050
1.0500 0.3270
1.1000 0.3590
1.2000 0.3730
1.4000 0.4180
1.6000 0.2750
Drag_induced
aero/qbar-psf
metrics/Sw-sqft
aero/cl-squared
aero/alpha-rad
velocities/mach
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
0.1750 0.1560 0.1500 0.1070 0.1050 0.1030 0.1020 0.1020 0.1010 0.0990 0.0980 0.1110 0.1600 0.1190
0.3490 0.6730 0.5730 0.4500 0.4510 0.4440 0.4430 0.4450 0.4430 0.4450 0.4470 0.6230 0.8560 0.7290
0.5240 1.4760 1.3320 1.1990 1.4870 1.5370 1.6100 1.6740 1.7090 1.7460 1.7740 1.9140 2.3430 1.9960
0.6980 2.1210 2.0970 2.8570 2.9140 2.9880 3.1060 3.2080 3.2780 3.3460 3.3770 3.5290 4.2260 3.5760
0.8730 2.5020 2.7550 4.5630 4.5610 4.6780 4.9210 5.1210 5.2740 5.4180 5.4270 5.5120 6.2080 5.3600
1.0470 2.9490 3.3400 6.2000 6.2250 6.3620 6.6550 6.8950 7.0660 7.2180 7.2770 7.4390 8.0250 7.1240
1.2220 3.2720 4.0200 7.6130 7.5170 7.6200 8.0050 8.3230 8.5590 8.7720 8.8950 9.0890 9.4860 8.6470
1.3960 3.4140 4.4490 8.5890 8.3450 8.5060 8.9530 9.3140 9.5900 9.8810 10.0510 10.1820 10.4330 9.7400
1.5530 3.3830 4.5250 8.9570 8.6620 8.8520 9.3210 9.6990 10.0120 10.3210 10.5040 10.5930 10.7020 10.1650
Side_force_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
aero/alpha-rad
velocities/mach
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 -4.5720 -4.7780 -2.8390 -2.7830 -2.7820 -2.7820 -2.8020 -2.7880 -2.7260 -2.6240 -2.1270 -3.7510 -1.8680
0.1750 -3.4650 -3.4620 -2.5390 -2.5700 -2.5920 -2.6220 -2.6620 -2.6740 -2.6870 -2.6990 -3.2400 -5.0870 -3.5300
0.3490 -4.0330 -3.1760 -2.3060 -2.4370 -2.4890 -2.5570 -2.6210 -2.6490 -2.7270 -2.8330 -4.4100 -6.4600 -5.2600
0.5240 -3.7880 -3.2320 -2.9470 -4.1930 -4.5100 -4.8660 -5.1520 -5.3400 -5.5510 -5.7630 -6.4010 -7.7820 -6.4780
0.6980 -3.1380 -3.0860 -4.9400 -5.1690 -5.4310 -5.7500 -6.0080 -6.2040 -6.4040 -6.5570 -6.9630 -7.8090 -6.5080
0.8730 -2.9750 -3.2000 -5.2580 -5.3000 -5.5000 -5.8190 -6.0770 -6.2740 -6.4640 -6.5150 -6.6640 -7.2910 -6.2470
1.0470 -2.7910 -3.0190 -4.9470 -4.9880 -5.1250 -5.3530 -5.5420 -5.6700 -5.7860 -5.8440 -6.0050 -6.4240 -5.6280
1.2220 -2.5860 -2.8680 -4.3030 -4.2850 -4.3540 -4.5250 -4.6730 -4.7700 -4.8570 -4.9100 -5.0550 -5.3130 -4.7050
1.3960 -2.3880 -2.5850 -3.4120 -3.3890 -3.4360 -3.5320 -3.6200 -3.6690 -3.7200 -3.7470 -3.8640 -4.0610 -3.5780
1.5530 -2.2370 -2.2840 -2.4930 -2.5160 -2.5300 -2.5510 -2.5830 -2.5840 -2.5840 -2.5790 -2.7030 -2.9020 -2.4700
Lift_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-rad
aero/alpha-rad
velocities/mach
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
0.1750 0.8920 0.8530 0.6050 0.5960 0.5830 0.5770 0.5780 0.5720 0.5640 0.5510 0.6290 0.0000 0.0000
0.3490 1.8910 1.5980 1.2390 1.2460 1.2240 1.2220 1.2310 1.2240 1.2300 1.2340 1.7500 0.9180 0.6530
0.5240 2.6800 2.3890 2.1310 2.7150 2.8200 2.9670 3.0950 3.1670 3.2450 3.3060 3.5860 2.3710 1.9530
0.6980 2.7130 2.6710 3.8650 3.9660 4.0880 4.2740 4.4320 4.5460 4.6580 4.7190 4.9500 4.0820 3.3810
0.8730 2.2200 2.4250 4.1130 4.1320 4.2580 4.4950 4.6880 4.8340 4.9760 5.0020 5.1060 5.0580 4.1590
1.0470 1.7770 1.9990 3.7420 3.7690 3.8700 4.0620 4.2180 4.3260 4.4280 4.4760 4.5890 5.2690 4.4650
1.2220 1.2300 1.5000 2.8490 2.8190 2.8740 3.0280 3.1540 3.2430 3.3290 3.3840 3.4650 4.7080 4.1210
1.3960 0.6120 0.7940 1.5350 1.4940 1.5310 1.6170 1.6850 1.7320 1.7870 1.8230 1.8500 3.5210 3.1700
1.5530 0.0470 0.0670 0.1450 0.1400 0.1440 0.1520 0.1590 0.1600 0.1650 0.1690 0.1720 1.8770 1.7320
Roll_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
aero/alpha-rad
velocities/mach
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
0.1750 0.1500 0.0890 0.0050 0.0110 0.0140 0.0160 0.0170 0.0170 0.0180 0.0190 0.0210 0.0370 0.0400
0.3490 -0.0550 -0.0550 -0.0370 -0.0290 -0.0270 -0.0240 -0.0220 -0.0200 -0.0160 -0.0100 0.0020 0.0350 0.0420
0.5240 -0.0280 -0.0200 0.0110 0.0160 0.0180 0.0190 0.0200 0.0210 0.0220 0.0180 0.0260 0.0500 0.0740
0.6980 0.2960 0.2760 0.2300 0.2210 0.2130 0.2090 0.2080 0.2040 0.1980 0.1880 0.1790 0.1560 0.1660
0.8730 0.3000 0.2920 0.2750 0.2730 0.2700 0.2690 0.2700 0.2680 0.2660 0.2610 0.2660 0.2690 0.2570
1.0470 0.2960 0.2980 0.3070 0.3110 0.3100 0.3110 0.3130 0.3120 0.3110 0.3080 0.3210 0.3390 0.3230
1.2220 0.3100 0.3120 0.3240 0.3290 0.3290 0.3300 0.3330 0.3320 0.3300 0.3280 0.3430 0.3650 0.3520
1.3960 0.3160 0.3170 0.3300 0.3360 0.3370 0.3380 0.3410 0.3400 0.3390 0.3380 0.3540 0.3780 0.3660
1.5530 0.3120 0.3130 0.3270 0.3320 0.3330 0.3340 0.3380 0.3370 0.3360 0.3340 0.3500 0.3740 0.3630
Pitch_moment_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-rad
aero/alpha-rad
velocities/mach
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 -1.3720 -1.7830 -1.3250 -0.2610 -0.2670 -0.0530 -0.2280 -0.1110 0.3980 -0.0010 -1.6930 -3.6220 9.0240
0.1750 -3.6990 -3.7670 -2.3840 -1.2630 -1.1680 -0.9210 -1.0390 -0.8730 -0.3300 -0.5070 -1.5380 -2.5500 8.7340
0.3490 -6.2840 -6.2120 -4.5940 -3.4430 -3.2580 -2.9880 -3.0420 -2.8720 -2.3760 -2.4010 -3.1630 -3.7190 5.6670
0.5240 -6.6830 -6.6450 -5.4900 -4.8850 -4.7620 -4.5880 -4.6300 -4.5470 -4.2660 -4.3030 -5.0530 -5.7670 0.4580
0.6980 -1.3220 -1.7460 -2.7300 -3.1210 -3.2820 -3.3450 -3.4360 -3.5030 -3.5630 -3.7900 -4.5880 -6.0190 -3.9490
0.8730 0.4270 -0.0950 -2.1340 -2.9000 -3.1370 -3.3200 -3.3910 -3.5370 -3.8170 -3.9870 -4.4190 -5.6210 -7.8500
1.0470 -3.0160 -3.0290 -4.1670 -4.9730 -5.0950 -5.2690 -5.2630 -5.4040 -5.7450 -5.6550 -5.4110 -5.5440 -11.3800
1.2220 -4.2180 -4.1060 -5.2920 -6.2680 -6.3560 -6.5490 -6.5100 -6.6640 -7.0630 -6.8850 -6.3960 -6.1490 -14.1200
1.3960 -4.5480 -4.4880 -5.7950 -6.8090 -6.8780 -7.0910 -7.0530 -7.2180 -7.6500 -7.4550 -6.9020 -6.5500 -15.1500
1.5530 -4.5480 -4.5460 -5.8850 -6.8540 -6.9290 -7.1500 -7.1170 -7.2760 -7.7250 -7.5390 -6.9700 -6.6060 -15.1600
Pitch_moment_due_to_pitch_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
velocities/q-aero-rad_sec
-50.0000
Pitch_moment_due_to_alpha_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
aero/alphadot-rad_sec
-3.4600
Yaw_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/beta-rad
aero/alpha-rad
velocities/mach
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 1.3720 1.7830 1.3250 0.2610 0.2670 0.0530 0.2280 0.1110 -0.3980 0.0010 1.6930 3.6220 -9.0240
0.1750 3.6990 3.7670 2.3840 1.2630 1.1680 0.9210 1.0390 0.8730 0.3300 0.5070 1.5380 2.5500 -8.7340
0.3490 6.2840 6.2120 4.5940 3.4430 3.2580 2.9880 3.0420 2.8720 2.3760 2.4010 3.1630 3.7190 -5.6670
0.5240 6.6830 6.6450 5.4900 4.8850 4.7620 4.5880 4.6300 4.5470 4.2660 4.3030 5.0530 5.7670 -0.4580
0.6980 1.3220 1.7460 2.7300 3.1210 3.2820 3.3450 3.4360 3.5030 3.5630 3.7900 4.5880 6.0190 3.9490
0.8730 -0.4270 0.0950 2.1340 2.9000 3.1370 3.3200 3.3910 3.5370 3.8170 3.9870 4.4190 5.6210 7.8500
1.0470 3.0160 3.0290 4.1670 4.9730 5.0950 5.2690 5.2630 5.4040 5.7450 5.6550 5.4110 5.5440 11.3800
1.2220 4.2180 4.1060 5.2920 6.2680 6.3560 6.5490 6.5100 6.6640 7.0630 6.8850 6.3960 6.1490 14.1200
1.3960 4.5480 4.4880 5.7950 6.8090 6.8780 7.0910 7.0530 7.2180 7.6500 7.4550 6.9020 6.5500 15.1500
1.5530 4.5480 4.5460 5.8850 6.8540 6.9290 7.1500 7.1170 7.2760 7.7250 7.5390 6.9700 6.6060 15.1600
Yaw_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
-60.0000