Erik Hofman
2005-01-01
$Revision: 1.31 $
McDonnell Douglas F-15 Eagle
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.). 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.
608
42.83
15.95
45.01
20
46.96
0
-234.15
0
0
-398.45
0
37
-237.25
0
4.58
28700
165100
187900
520
28000
-236.39
0
4.5
230
-398.45
0
20
-393.2
0
-89.2
0.8
0.5
0.02
12200
5000
5
NONE
1
-187
-54
-85.4
0.8
0.5
0.02
22704
9000
0.0
LEFT
1
-187
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-85.4
0.8
0.5
0.02
22704
9000
0.0
RIGHT
1
-92.2
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0.2
0.2
0.2
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2000
0.0
NONE
0
-92.2
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0.2
0.2
0.2
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2000
0.0
NONE
0
47.4
-69.7
133.8
0.2
0.2
0.2
10000
2000
0.0
NONE
0
47.4
69.7
133.8
0.2
0.2
0.2
10000
2000
0.0
NONE
0
-648.7
0
-17
0.2
0.2
0.2
10000
2000
0.0
NONE
0
-187
0
-37
0.2
0.2
0.2
10000
2000
0.0
NONE
0
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-25.5
0
0.0
0
0
0
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50
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0
0.0
0.0
0.0
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0.0
0.0
0.0
-236.39
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4.5
6561.5
2500
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0
4.5
6561.5
2500
fcs/elevator-cmd-norm
fcs/pitch-trim-cmd-norm
-1
1
fcs/pitch-trim-sum
-1
1
fcs/pitch-trim-sum
0.01745
-1
1
-26
15
fcs/aileron-cmd-norm
fcs/roll-trim-cmd-norm
-1
1
fcs/roll-trim-sum
-1
1
fcs/aileron-pos-norm
0.01745
-20
20
fcs/aileron-pos-norm
-0.01745
-20
20
velocities/r-rad_sec
-0.001745
fcs/rudder-cmd-norm
fcs/yaw-trim-cmd-norm
fcs/yaw-damper-gain
-1
1
fcs/yaw-trim-sum
-1
1
fcs/rudder-pos-norm
0.01745
-30
30
gear/gear-cmd-norm
0
1
fcs/speedbrake-cmd-norm
0
1
Change_in_lift_due_to_ground_effect
aero/h_b-mac-ft
0.0000 1.0610
0.1000 1.0330
0.1500 1.0310
0.2000 1.0330
0.3000 1.0280
0.4000 1.0110
0.5000 1.0090
0.6000 1.0050
0.7000 1.0020
0.8000 1.0000
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
Change_in_drag_due_to_ground_effect
aero/h_b-mac-ft
0.0000 0.8100
0.1000 0.9900
0.1500 0.9500
0.2000 0.9800
0.3000 0.9900
0.4000 1.0000
0.5000 1.0400
0.6000 1.0100
0.7000 0.9900
0.8000 1.0100
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
Change_in_pitch_due_to_ground_effect
aero/h_b-mac-ft
0.0000 0.9920
0.1000 0.9960
0.1500 0.9990
0.2000 0.9970
0.3000 1.0000
0.4000 1.0000
0.5000 1.0020
0.6000 1.0010
0.7000 0.9980
0.8000 0.9990
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
Drag_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/function/kCDge
aero/alpha-rad
velocities/mach
0.5000 1.4000
-0.4190 0.3800 0.0970
-0.2790 0.2200 0.0250
-0.1400 0.0700 0.0180
-0.0700 0.0400 0.0100
0.0000 0.0147 0.0074
0.0700 0.0400 0.0100
0.1400 0.0700 0.0180
0.2790 0.2200 0.0250
0.4190 0.3800 0.0970
0.5590 0.8000 0.2030
0.6980 1.0100 0.2570
Drag_induced
aero/qbar-psf
metrics/Sw-sqft
aero/function/kCDge
aero/alpha-rad
-0.3490 0.2270
-0.2620 0.0670
-0.1750 0.0480
-0.0870 0.0060
0.0000 0.0060
0.0700 0.0130
0.1400 0.0200
0.2090 0.0470
0.2790 0.0670
0.3490 0.2120
0.4190 0.2270
0.4890 0.3310
0.5590 0.4740
0.6980 0.2120
0.7850 0.9130
0.8730 0.7210
Drag_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
aero/mag-beta-rad
aero/function/kCDge
aero/alpha-rad
-0.3490 2.5954
-0.2620 3.2686
-0.1750 3.3563
-0.0870 3.0533
0.0000 3.8228
0.0700 4.3450
0.1400 4.1909
0.2090 3.7331
0.2790 3.1268
0.3490 2.8246
0.4190 2.4657
0.4890 2.2127
0.5590 1.9317
0.6980 1.2283
0.7850 0.9522
0.8730 0.7015
Drag_due_to_Elevator_Deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/mag-elevator-pos-rad
0.0438
Side_force_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
aero/alpha-rad
-0.3490 -0.8594
0.0700 -0.0974
0.5590 -0.0115
0.8730 -0.3552
Side_force_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
fcs/left-aileron-pos-rad
-0.0012
Side_force_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
fcs/rudder-pos-rad
0.3724
Lift_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/function/kCLge
aero/alpha-rad
velocities/mach
0.5000 1.4000
-0.3490 -0.9300 -0.2500
-0.2620 -0.8600 -0.2300
-0.1750 -0.5800 -0.1600
-0.0870 -0.2600 -0.0700
0.0000 0.0600 0.0200
0.0700 0.3000 0.0800
0.1400 0.5800 0.1600
0.2090 0.7800 0.2100
0.2790 0.8800 0.2400
0.3490 1.0100 0.2700
0.4190 1.0800 0.2900
0.4890 1.1600 0.3100
0.5590 1.1900 0.3200
0.6980 1.1700 0.3100
0.7850 1.0900 0.2900
0.8730 1.0500 0.2800
Lift_due_to_Elevator_Deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/elevator-pos-rad
0.5730
Lift_due_to_alpha_rate
aero/qbar-psf
metrics/Sw-sqft
aero/alphadot-rad_sec
aero/ci2vel
17.2232
Lift_due_to_pitch_rate
aero/qbar-psf
metrics/Sw-sqft
velocities/q-aero-rad_sec
aero/ci2vel
-17.2232
Roll_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
aero/alpha-rad
-0.3490 0.0286
-0.1750 -0.2292
0.0000 -0.0573
0.2090 -0.1719
0.3140 -0.1146
0.4190 -0.1719
0.6980 -0.0745
0.7850 -0.1146
0.8730 -0.1203
Roll_moment_due_to_roll_rate_(roll_damping)
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
aero/alpha-rad
0.0000 -0.4000
0.3490 -0.3100
Roll_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
0.0001
Roll_moment_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
aero/alpha-rad
-0.3490 0.0172
-0.0870 0.0372
0.1400 0.0401
0.5590 0.0057
0.8730 0.0057
Roll_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
0.0115
Pitch_moment_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-rad
aero/function/kCmge
aero/alpha-rad
-0.3490 -1.1459
-0.2620 -0.5730
-0.1310 -0.0573
0.0000 -0.2292
0.2790 -0.5157
0.4190 -0.8594
0.5590 -0.4584
0.8730 -0.5157
Pitch_moment_due_to_alpha_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
aero/alphadot-rad_sec
-11.8870
Pitch_moment_due_to_Mach
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
velocities/mach
-0.0000
Pitch_moment_due_to_pitch_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
velocities/q-aero-rad_sec
-4.7000
Pitch_moment_due_to_elevator_deflection
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
fcs/elevator-pos-rad
-0.4580
Yaw_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
aero/alpha-rad
-0.3490 0.0745
0.0000 0.1776
0.3490 0.0057
0.5240 -0.0974
0.8730 -0.0286
Yaw_moment_due_to_roll_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
aero/alpha-rad
-0.3490 0.1100
-0.0870 -0.1400
0.0000 -0.1000
0.2790 0.0100
0.4190 -0.1300
0.8730 -0.1800
Yaw_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
-0.4447
Yaw_moment_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
0.0022
Yaw_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
aero/alpha-rad
-0.3490 -0.0688
0.8730 -0.0115