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Text File  |  1993-12-19  |  5KB  |  75 lines
  1.  ENHANCED AIRCRAFT DESIGNER - MAIN MENU                                         
  2.  
  3.  Menus                                  Main Wings                              
  4.    A  STABILIZER SYSTEMS...               J  Span In Feet;00036                 
  5.                                           K  Chord In Feet;00005                
  6.    C  WGT/BAL/INSTRUM/STRUCT...           L  Aspect Ratio;007.20                
  7.    D  AERODYNAMICS/CONTROLS...            M  Angle Of Incidence;000.00          
  8.                                           N  Induced Drag Adj.;13107            
  9.                                           O  Dihedral (Degrees);00004           
  10.  Files                                    P  Dihedral Scale;00100               
  11.    F  Write Flight Parameter File         Q  Gyro Dihedral;00050                
  12.    G  Filename; PA-38-11                  R  Winglets                           
  13.    H  Aircraft Name; PA-38-112 Piper Tomahawk                                   
  14.    I  Save Aircraft To Disk             Airframe And Propulsion                 
  15.                                           S  Type:  PROP                        
  16.                                           T  Power: HP    00112                 
  17.                                           U  Altitude Derate;00060              
  18.  
  19.  
  20.  STABILIZER SYSTEMS                                                             
  21.  
  22.  Horizontal Stabilizer                  Damping Effects                         
  23.    A  Position;00270                      G  Pitch Damper;00015                 
  24.    B  Surface Area;00040                  H  Roll Damper;00000                  
  25.    C  Angle Of Incidence;008.24           I  Yaw Damper;16000                   
  26.    D  Lift Coefficient Scale;16384        J  Pitch Vel. Hyst.;00080             
  27.                                                                                 
  28.  Tail                                   Stability Augmentation                  
  29.    E  Position;00315                      K  Pitch Stabilizer Easy;32000        
  30.    F  Surface Area;00015                  L  Pitch Stabilizer Real;10000        
  31.  
  32.  
  33.  COLOR AND VISUAL DESIGN                                                        
  34.  
  35.  VISUAL EFFECTS                                                                 
  36.    K  Aircraft Numbers ; N4081L                                                 
  37.  
  38.  
  39.  WEIGHT/BALANCE/INSTRUMENTS/STRUCTURE                                           
  40.  
  41.  Weight And Balance                      Instruments                            
  42.    A  Dry Weight LBS;01170                 H  Overspeed Warning;00138           
  43.    B  Fuel Capacity GAL;00032              I  Sim Switches;00000                
  44.    C  Center Of Gravity;00095              J  Stall Warning Angle;008.99        
  45.    D  Center Of Lift;00108                 K  Enhanced Instrument Panel         
  46.    E  Pitch Inverse Moment;20000                                                
  47.    F  Roll Inverse Moment;06000          Structure                              
  48.    G  Yaw Inverse Moment;10000             L  Gear: Retractable                 
  49.                                            M  Canard Configuration              
  50.  
  51.  
  52.  AERODYNAMICS/CONTROLS                 N  Crash Resistance;00008                
  53.  
  54.  Surface Areas                            Control Sensitivities                 
  55.    A  Frontal Area (Sq. Ft.);00005          M  Rudder Sens.;08000               
  56.    B  Frontal Area Scale;00005              N  Rudder Half;00200                
  57.    C  Body Side Area;00320                  O  Rudder Eighth;01000              
  58.                                             P  Ailer. Sens.;01400               
  59.  Flaps Lift/Drag Coefficients               Q  Ailer. Half;00200                
  60.    D  Flaps Lift Coef.;08192                R  Ailer. Eighth;01000              
  61.    E  Flaps Drag Coef.;00490                S  Elev. Half;00200                 
  62.                                             T  Elev. Eighth;01000               
  63.  Drag Coefficients                          U  Ground Steering;00000            
  64.    F  Gear Drag Coef.;00000                                                     
  65.    G  Slow Speed Drag;00008               Miscellaneous.                        
  66.    H  Spoiler Drag;00000                    V  Stall Synthesize;00028           
  67.    I  Touchdown Drag;00050                  W  Heavy Aircraft                   
  68.    J  Slip Drag;00012                       Y  Thrust Reversers                 
  69.                                                                                 
  70.  Dynamic Pressure Effects                                                       
  71.    K  Max Velocity;00240                                                        
  72.    L  Dynamic Pressure Limit;00075                                              
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