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C!T ROM 2
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FLIGHTSI
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PL_737-3
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BOEINGB7.PRF
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Text File
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1992-12-08
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5KB
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75 lines
ENHANCED AIRCRAFT DESIGNER - MAIN MENU
Menus Main Wings
A STABILIZER SYSTEMS... J Span In Feet;00213
K Chord In Feet;00030
C WGT/BAL/INSTRUM/STRUCT... L Aspect Ratio;006.99
D AERODYNAMICS/CONTROLS... M Angle Of Incidence;352.99
N Induced Drag Adj.;16384
O Dihedral (Degrees);00002
Files P Dihedral Scale;00100
F Write Flight Parameter File Q Gyro Dihedral;00050
G Filename; BOEINGB7 R +Winglets
H Aircraft Name; BOEING B737-300
I Save Aircraft To Disk Airframe And Propulsion
S Type: JET
T Power: LBS 00095 x 1000
U Altitude Derate;00536
STABILIZER SYSTEMS
Horizontal Stabilizer Damping Effects
A Position;02310 G Pitch Damper;00250
B Surface Area;01243 H Roll Damper;30000
C Angle Of Incidence;000.00 I Yaw Damper;65000
D Lift Coefficient Scale;15384 J Pitch Vel. Hyst.;00000
Tail Stability Augmentation
E Position;02142 K Pitch Stabilizer Easy;20000
F Surface Area;00932 L Pitch Stabilizer Real;10000
COLOR AND VISUAL DESIGN
VISUAL EFFECTS
K Aircraft Numbers ;
WEIGHT/BALANCE/INSTRUMENTS/STRUCTURE
Weight And Balance Instruments
A Dry Weight LBS x 1000;00075 H Overspeed Warning;00550
B Fuel Tanks LBS x 1000;00120 I Sim Switches;00002
C Center Of Gravity;01100 J Stall Warning Angle;011.99
D Center Of Lift;01260 K Enhanced Instrument Panel
E Pitch Inverse Moment;01000
F Roll Inverse Moment;00425 Structure
G Yaw Inverse Moment;05000 L Gear: Fixed
M Canard Configuration
AERODYNAMICS/CONTROLS N Crash Resistance;00015
Surface Areas Control Sensitivities
A Frontal Area (Sq. Ft.);00100 M Rudder Sens.;08000
B Frontal Area Scale;00200 N Rudder Half;00300
C Body Side Area;09600 O Rudder Eighth;01500
P Ailer. Sens.;01500
Flaps Lift/Drag Coefficients Q Ailer. Half;00500
D Flaps Lift Coef.;05000 R Ailer. Eighth;02500
E Flaps Drag Coef.;00150 S Elev. Half;00150
T Elev. Eighth;00600
Drag Coefficients U Ground Steering;03000
F Gear Drag Coef.;00060
G Slow Speed Drag;00040 Miscellaneous.
H Spoiler Drag;00300 V Stall Synthesize;00044
I Touchdown Drag;00175 W +Heavy Aircraft
J Slip Drag;00010 Y +Thrust Reversers
Dynamic Pressure Effects
K Max Velocity;00610
L Dynamic Pressure Limit;00200