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C!T ROM 2
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FLIGHTSI
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VLIEGTUI
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PL_F-50
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FOKKER50.PRF
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Text File
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1992-12-21
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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;00054
K Chord In Feet;00005
C WGT/BAL/INSTRUM/STRUCT... L Aspect Ratio;009.99
D AERODYNAMICS/CONTROLS... M Angle Of Incidence;354.99
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; FOKKER50 R +Winglets
H Aircraft Name; FOKKER 50 TURBO-PROP
I Save Aircraft To Disk Airframe And Propulsion
S Type: PROP
T Power: HP 03000
U Altitude Derate;00031
STABILIZER SYSTEMS
Horizontal Stabilizer Damping Effects
A Position;00059 G Pitch Damper;00225
B Surface Area;00061 H Roll Damper;30000
C Angle Of Incidence;000.00 I Yaw Damper;65000
D Lift Coefficient Scale;16384 J Pitch Vel. Hyst.;00000
Tail Stability Augmentation
E Position;00446 K Pitch Stabilizer Easy;02000
F Surface Area;00014 L Pitch Stabilizer Real;04000
COLOR AND VISUAL DESIGN
VISUAL EFFECTS
K Aircraft Numbers ;
WEIGHT/BALANCE/INSTRUMENTS/STRUCTURE
Weight And Balance Instruments
A Dry Weight LBS;09000 H Overspeed Warning;00325
B Fuel Capacity GAL;00500 I Sim Switches;00002
C Center Of Gravity;00280 J Stall Warning Angle;011.99
D Center Of Lift;00325 K Enhanced Instrument Panel
E Pitch Inverse Moment;02000
F Roll Inverse Moment;02000 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.);00015 M Rudder Sens.;08000
B Frontal Area Scale;00010 N Rudder Half;00300
C Body Side Area;00448 O Rudder Eighth;01500
P Ailer. Sens.;00750
Flaps Lift/Drag Coefficients Q Ailer. Half;00500
D Flaps Lift Coef.;05000 R Ailer. Eighth;02500
E Flaps Drag Coef.;01500 S Elev. Half;00150
T Elev. Eighth;00600
Drag Coefficients U Ground Steering;03000
F Gear Drag Coef.;00200
G Slow Speed Drag;00080 Miscellaneous.
H Spoiler Drag;00300 V Stall Synthesize;00044
I Touchdown Drag;00150 W Heavy Aircraft
J Slip Drag;00010 Y Thrust Reversers
Dynamic Pressure Effects
K Max Velocity;00400
L Dynamic Pressure Limit;00200