home
***
CD-ROM
|
disk
|
FTP
|
other
***
search
/
C!T ROM 2
/
ctrom_ii_b.zip
/
ctrom_ii_b
/
FLIGHTSI
/
VLIEGTUI
/
PL_BLERI
/
XI-2-AAF.PRF
< prev
next >
Wrap
Text File
|
1993-02-13
|
5KB
|
75 lines
ENHANCED AIRCRAFT DESIGNER - MAIN MENU
Menus Main Wings
A STABILIZER SYSTEMS... J Span In Feet;00040
K Chord In Feet;00005
C WGT/BAL/INSTRUM/STRUCT... L Aspect Ratio;007.99
D AERODYNAMICS/CONTROLS... M Angle Of Incidence;005.99
N Induced Drag Adj.;05000
O Dihedral (Degrees);00003
Files P Dihedral Scale;00100
F Write Flight Parameter File Q Gyro Dihedral;00050
G Filename; XI-2(AAF R Winglets
H Aircraft Name; XI-2 (aaf source SIM)
I Save Aircraft To Disk Airframe And Propulsion
S Type: PROP
T Power: HP 00080
U Altitude Derate;00030
STABILIZER SYSTEMS
Horizontal Stabilizer Damping Effects
A Position;00251 G Pitch Damper;00015
B Surface Area;00027 H Roll Damper;00000
C Angle Of Incidence;000.00 I Yaw Damper;16000
D Lift Coefficient Scale;15000 J Pitch Vel. Hyst.;00080
Tail Stability Augmentation
E Position;00262 K Pitch Stabilizer Easy;32000
F Surface Area;00011 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;00800 H Overspeed Warning;00100
B Fuel Capacity GAL;00050 I Sim Switches;00002
C Center Of Gravity;00075 J Stall Warning Angle;011.99
D Center Of Lift;00098 K Enhanced Instrument Panel
E Pitch Inverse Moment;20000
F Roll Inverse Moment;06000 Structure
G Yaw Inverse Moment;10000 L Gear: JET
M Canard Configuration
AERODYNAMICS/CONTROLS N Crash Resistance;00151
Surface Areas Control Sensitivities
A Frontal Area (Sq. Ft.);00007 M Rudder Sens.;08000
B Frontal Area Scale;00010 N Rudder Half;00250
C Body Side Area;00200 O Rudder Eighth;01250
P Ailer. Sens.;01000
Flaps Lift/Drag Coefficients Q Ailer. Half;00350
D Flaps Lift Coef.;00000 R Ailer. Eighth;01750
E Flaps Drag Coef.;00000 S Elev. Half;00250
T Elev. Eighth;01250
Drag Coefficients U Ground Steering;00000
F Gear Drag Coef.;00100
G Slow Speed Drag;00035 Miscellaneous.
H Spoiler Drag;00000 V Stall Synthesize;00020
I Touchdown Drag;00020 W Heavy Aircraft
J Slip Drag;00011 Y Thrust Reversers
Dynamic Pressure Effects
K Max Velocity;00200
L Dynamic Pressure Limit;00050