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Text File  |  1992-12-12  |  5KB  |  75 lines
  1.  ENHANCED AIRCRAFT DESIGNER - MAIN MENU                                         
  2.  
  3.  Menus                                  Main Wings                              
  4.    A  STABILIZER SYSTEMS...               J  Span In Feet;00022                 
  5.                                           K  Chord In Feet;00010                
  6.    C  WGT/BAL/INSTRUM/STRUCT...           L  Aspect Ratio;002.20                
  7.    D  AERODYNAMICS/CONTROLS...            M  Angle Of Incidence;004.99          
  8.                                           N  Induced Drag Adj.;16384            
  9.                                           O  Dihedral (Degrees);00006           
  10.  Files                                    P  Dihedral Scale;00100               
  11.    F  Write Flight Parameter File         Q  Gyro Dihedral;00050                
  12.    G  Filename; F104M1                    R  Winglets                           
  13.    H  Aircraft Name; F104 M1                                                    
  14.    I  Save Aircraft To Disk             Airframe And Propulsion                 
  15.                                           S  Type:  JET                         
  16.                                           T  Power: LBS   17800                 
  17.                                           U  Altitude Derate;00250              
  18.  
  19.  
  20.  STABILIZER SYSTEMS                                                             
  21.  
  22.  Horizontal Stabilizer                  Damping Effects                         
  23.    A  Position;00540                      G  Pitch Damper;00100                 
  24.    B  Surface Area;00060                  H  Roll Damper;30000                  
  25.    C  Angle Of Incidence;000.00           I  Yaw Damper;65000                   
  26.    D  Lift Coefficient Scale;16384        J  Pitch Vel. Hyst.;00080             
  27.                                                                                 
  28.  Tail                                   Stability Augmentation                  
  29.    E  Position;00550                      K  Pitch Stabilizer Easy;00000        
  30.    F  Surface Area;00035                  L  Pitch Stabilizer Real;00000        
  31.  
  32.  
  33.  COLOR AND VISUAL DESIGN                                                        
  34.  
  35.  VISUAL EFFECTS                                                                 
  36.    K  Aircraft Numbers ; 53-04                                                  
  37.  
  38.  
  39.  WEIGHT/BALANCE/INSTRUMENTS/STRUCTURE                                           
  40.  
  41.  Weight And Balance                      Instruments                            
  42.    A  Dry Weight LBS;14082                 H  Overspeed Warning;01460           
  43.    B  Fuel Capacity GAL;00700              I  Sim Switches;00000                
  44.    C  Center Of Gravity;00350              J  Stall Warning Angle;009.99        
  45.    D  Center Of Lift;00360                 K  Enhanced Instrument Panel         
  46.    E  Pitch Inverse Moment;05000                                                
  47.    F  Roll Inverse Moment;10000          Structure                              
  48.    G  Yaw Inverse Moment;05000             L  Gear: Fixed                       
  49.                                            M  Canard Configuration              
  50.  
  51.  
  52.  AERODYNAMICS/CONTROLS                 N  Crash Resistance;00012                
  53.  
  54.  Surface Areas                            Control Sensitivities                 
  55.    A  Frontal Area (Sq. Ft.);00011          M  Rudder Sens.;08000               
  56.    B  Frontal Area Scale;00011              N  Rudder Half;00300                
  57.    C  Body Side Area;00480                  O  Rudder Eighth;02000              
  58.                                             P  Ailer. Sens.;00750               
  59.  Flaps Lift/Drag Coefficients               Q  Ailer. Half;00600                
  60.    D  Flaps Lift Coef.;08192                R  Ailer. Eighth;02500              
  61.    E  Flaps Drag Coef.;00500                S  Elev. Half;00800                 
  62.                                             T  Elev. Eighth;03000               
  63.  Drag Coefficients                          U  Ground Steering;00000            
  64.    F  Gear Drag Coef.;00200                                                     
  65.    G  Slow Speed Drag;00020               Miscellaneous.                        
  66.    H  Spoiler Drag;00000                    V  Stall Synthesize;00044           
  67.    I  Touchdown Drag;00150                  W  Heavy Aircraft                   
  68.    J  Slip Drag;00010                       Y  Thrust Reversers                 
  69.                                                                                 
  70.  Dynamic Pressure Effects                                                       
  71.    K  Max Velocity;01500                                                        
  72.    L  Dynamic Pressure Limit;00250                                              
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