Aeromatic v 0.9, refined by Jon Berndt
2008-12-22
$Revision: 1.8 $
Models a Boeing B-17G.
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.
1420.00
103.75
2.00
13.69
22.50
0.00
0.00
11.0
-2.0
3.5
0.0
0.0
0.0
400000
250000
600000
36100
22.0
0.0
-0.5
20.9
-10.0
-8.5
0.80
0.50
0.02
30000.00
3000.00
0
LEFT
1
20.9
10.0
-8.5
0.80
0.50
0.02
30000.00
3000.00
0
RIGHT
1
52.5
0.00
-4.75
0.80
0.50
0.02
6500.0
650.00
5.00
NONE
1
24.0
-51.9
1.9
0.80
0.50
65500.00
13100.00
24.0
51.9
1.9
0.80
0.50
65500.00
13100.00
10.1
-21.6
-0.4
0
1
2
3
4
9
10.1
-21.6
-0.4
0
0
0
8.6
-10.0
-0.7
5
6
7
8
10
11
8.6
-10.0
-0.7
0
0
0
8.6
10.0
-0.7
12
13
15
16
17
18
8.6
10.0
-0.7
0
0
0
10.1
21.6
-0.4
14
19
20
21
22
23
10.1
21.6
-0.4
0
0
0
B-17 Pilot's Manual "Left Outboard Tank 1" (54 US Gallons)
24.7
-45.8
2.0
328
328
B-17 Pilot's Manual "Left Outboard Tank 2" (54 US Gallons)
24.7
-43.8
2.0
328
328
B-17 Pilot's Manual "Left Outboard Tank 3" (54 US Gallons)
24.7
-41.9
2.0
328
328
B-17 Pilot's Manual "Left Outboard Tank 4" (54 US Gallons)
24.7
-40.0
2.0
328
328
B-17 Pilot's Manual "Left Outboard Tank 5" (54 US Gallons)
24.7
-37.7
2.0
328
328
B-17 Pilot's Manual "Left Inboard Tank 6" (67.5 US Gallons)
24.7
-35.8
2.0
410
410
B-17 Pilot's Manual "Left Inboard Tank 7" (67.5 US Gallons)
24.7
-33.9
2.0
410
410
B-17 Pilot's Manual "Left Inboard Tank 8" (67.5 US Gallons)
24.7
-32.0
2.0
410
410
B-17 Pilot's Manual "Left Inboard Tank 9" (67.5 US Gallons)
24.7
-30.1
2.0
410
410
B-17 Pilot's Manual "Left Outboard Engine tank" (425 US Gallons)
22.4
-25.8
1.0
2581
2581
B-17 Pilot's Manual "Left Inboard Engine tank" (213 US Gallons)
22.4
-14.3
1.0
1293
1293
B-17 Pilot's Manual "Left Inboard Engine 2 Feeder tank" (212 US Gallons)
25.0
-14.3
1.0
1287
1287
B-17 Pilot's Manual "Right Inboard Engine Feeder tank" (212 US Gallons)
25.0
14.3
1.0
1287
1287
B-17 Pilot's Manual "Right Inboard Engine tank" (213 US Gallons)
22.4
14.3
1.0
1293
1293
B-17 Pilot's Manual "Right Outboard Engine tank" (425 US Gallons)
22.4
25.8
1.0
2581
2581
B-17 Pilot's Manual "Right Inboard Tank 9" (67.5 US Gallons)
24.7
30.1
2.0
410
410
B-17 Pilot's Manual "Rightt Inboard Tank 8" (67.5 US Gallons)
24.7
32.0
2.0
410
410
B-17 Pilot's Manual "Right Inboard Tank 7" (67.5 US Gallons)
24.7
33.9
2.0
410
410
B-17 Pilot's Manual "Right Inboard Tank 6" (67.5 US Gallons)
24.7
35.8
2.0
410
410
B-17 Pilot's Manual "Right Outboard Tank 5" (54 US Gallons)
24.7
37.7
2.0
328
328
B-17 Pilot's Manual "Right Outboard Tank 4" (54 US Gallons)
24.7
40.0
2.0
328
328
B-17 Pilot's Manual "Right Outboard Tank 3" (54 US Gallons)
24.7
41.9
2.0
328
328
B-17 Pilot's Manual "Right Outboard Tank 2" (54 US Gallons)
24.7
43.8
2.0
328
328
B-17 Pilot's Manual "Right Outboard Tank 1" (54 US Gallons)
24.7
45.8
2.0
328
328
fcs/elevator-cmd-norm
fcs/pitch-trim-cmd-norm
-1
1
fcs/pitch-trim-sum
-0.35
0.35
fcs/elevator-pos-rad
-0.35
0.35
-1
1
fcs/aileron-cmd-norm
fcs/roll-trim-cmd-norm
-1
1
fcs/roll-trim-sum
-0.35
0.35
fcs/roll-trim-sum
-0.35
0.35
fcs/left-aileron-pos-rad
-0.35
0.35
-1
1
fcs/right-aileron-pos-rad
-0.35
0.35
-1
1
fcs/rudder-cmd-norm
fcs/yaw-trim-cmd-norm
-0.35
0.35
fcs/rudder-command-sum
-0.35
0.35
fcs/rudder-pos-rad
-0.35
0.35
-1
1
fcs/flap-cmd-norm
0
15
30
fcs/flap-pos-deg
0
30
0
1
gear/gear-cmd-norm
0
1
fcs/speedbrake-cmd-norm
0
1
This parameter calculates the angle of attack at the right wingtip,
accounting for the motion of the wing at that point away from the CG.
velocities/w-fps
velocities/p-aero-rad_sec
50
velocities/u-fps
velocities/r-aero-rad_sec
50
Lift_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-rad
-0.20 -0.740
0.00 0.240
0.24 1.400
0.60 0.704
Delta_Lift_due_to_flaps
aero/qbar-psf
metrics/Sw-sqft
fcs/flap-pos-deg
0.02000
Delta_Lift_due_to_speedbrake
aero/qbar-psf
metrics/Sw-sqft
fcs/speedbrake-pos-norm
0
Lift_due_to_Elevator_Deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/elevator-pos-rad
0.2
Drag_at_zero_lift
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-rad
-1.57 1.500
-0.26 0.033
0.00 0.025
0.26 0.033
1.57 1.500
Induced_drag
aero/qbar-psf
metrics/Sw-sqft
aero/cl-squared
0.039
Drag_due_to_mach
aero/qbar-psf
metrics/Sw-sqft
velocities/mach
0.00 0.000
0.7 0.000
1.10 0.023
1.80 0.015
Drag_due_to_flaps
aero/qbar-psf
metrics/Sw-sqft
fcs/flap-pos-deg
0.00117
Drag_due_to_gear
aero/qbar-psf
metrics/Sw-sqft
gear/gear-pos-norm
0.023
Drag_due_to_speedbrakes
aero/qbar-psf
metrics/Sw-sqft
fcs/speedbrake-pos-norm
0.025
Drag_due_to_sideslip
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
Drag_due_to_Elevator_Deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/elevator-pos-norm
0.04
Side_force_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
-1
Roll_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
-0.1
Roll_moment_due_to_roll_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
-0.4
Roll_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
0.15
Roll_moment_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
velocities/mach
0.0 0.150
2.0 0.050
Roll_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
0.01
Pitch_moment_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-rad
-0.4
Pitch_moment_due_to_elevator
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
fcs/elevator-pos-rad
velocities/mach
0.0 -1.000
2.0 -0.250
Pitch_moment_due_to_pitch_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
velocities/q-aero-rad_sec
-22
Pitch_moment_due_to_alpha_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
aero/alphadot-rad_sec
-8
Yaw_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
0.12
Yaw_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
-0.15
Yaw_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
-0.1
Adverse_yaw
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
-0.008