Aircraft  1.1
=================================================================================================
   ,  -                .
       Excel  +  VBA
                        
            .
              !!!

  <Speed>
=================================================================================================
              
                  
                 .

  <Data>  
=================================================================================================
            

   <Cy  >     <Cx  >  
            0    25   
              1    45  
   -154             15 - 28 - 36 - 45 

   <Cy >     <Cx>   
                    0   25   
           ( 0,00  -  2,40 ) 

   <Cr>                        
   <Pmax>                        
   <K>                     
    <V>                   



  <Loading>  
=================================================================================================
                 
                 
                 
            . 
          -154
        .
          3      100 / 200 / 300 
                    
                      "H".  
           -154

      
           4        10000   
     -154  
        1        6500 
        2        5000 
        3   0  
        4   0  

  
             
3         20 000     
2             50 000    
2             25 000    
2             15 000    
       240 000 

            -154  
       2                 ( -154    4       6600    )
       3                 ( -154    1   3300   )  
          ( -154    2      19000   )
               ( -154    3      10850   )

                  
           %           24     32  (     28  )   


  <Cockpit>
=================================================================================================

      .           .
             
-       
-     
-      
-      (  )    .

             
                        
(       )      
                       
(        )      
               
                 H1      H2  .
                Vy        (        )
                
              
                         
                          

                  
           (  )  
            (  )  
          0    100 %               10 %
  -              %             
    ""         1    45              
    <Cy >   <Cx >       Data            
           
                     

                  2 - 3  
                  1 - 2 - 3 
           2 - 3 - 4 - 5

           (  )        
    0    -30     
      0    +30   

        (  )        
    0    -10   
      0    +10   

     (  )                   0    30 000 

                          FMC    
(               ) 

DVP  -  Diagram  of  the  Vertical  Profile 
     FMC              
          (        )   
         (        )   
      DVP  
                     
                              BSDR
                     
                       
            
                     10 -        

           FMC        
                

GWD  -  Geometric  Wing   Data  -        
GHSD  -  Geometric   Horizontal   Stabilizer   Data  -           
GVSD  -  Geometric   Vertical   Stabilizer   Data  -           
GFD  -  Geometric   Fuselage   Data  -        
ADD  -  Aero Dinamic Data  -     


GWD  -  Geometric  Wing   Data  -        
     Geometric  Wing   Data          GWD
     74     M74                  





             -154
                            
     OK  
              .


GHSD  -  Geometric   Horizontal   Stabilizer   Data  -           
     Geometric   Horizontal   Stabilizer   Data          GHSD
     74    P74                   





             -154
                            
     OK  
              .


GVSD  -  Geometric   Vertical   Stabilizer   Data  -           
     Geometric   Vertical   Stabilizer   Data          GVSD
             -154
                            
     OK  
              .


GFD  -  Geometric   Fuselage   Data  -        
     Geometric   Fuselage   Data          GFD
    74      I74                    
      .      <   >   

1 -         		
2 -          		
3 -          		
4 -          		
5 -       		
6 -            		
	
             -154
                            
     OK  
              .

                
                   
     .           
              > 1  


ADD  -  Aero Dinamic Data  -     
     Aero Dinamic Data         ADD
             -154
                       
     OK  
              .


START -      
      Start          START
                           
                    OK   
                        OK
     O           .


ND -  NavData  -    
    NavData        ND
                  
                  
                  
    OK                 
               .
                  
                Cockpit
        (  ) -       
       (  ) -   
                      
    ,                
    /   ,     ,    / 


PLAN - Flight Plan -      
     Flight Plan         PLAN
       36        36                  
                   (  1 ) 
                                  (  2 )  
                 
            OK  
                        
           FMC  


ENG - Engine -    
    Engine         ENG
                  
             -30-154
    74      H74              

    
 

   <>                   Pmax      Data
   <>           Pmax      
                  Pmax      
     <>                
       ,       
                  
     OK  
              .


FLIGHT -       
    Flight         FLIGHT
                      ""
                   
                        <Loading>  
                            
                        "0"   
                      
     OK   
              .


LANDING -        
     Landing      LANDING
                     ""
                   
                              
                             
                           
                        "0"   
                  
     OK  
               .


BSDR  -  Board  System  Data  Recording  -            

         BSDR                           
        NavData   
                    
     OK                  
               .

                     
           Board  System  Data  Recording       BSDR   
     OK                    
              .
                           BSDR 
            .
               .


ADF  -   Aero Dinamic Focus  -     
     Aero Dinamic Focus        ADF  
                     
         
         
      
                         
                      
     OK        
               .



LSTAB  -  Long   Stability  -    
         Long   Stability           
          ADF
     Long   Stability         LSTAB  
                         Cm0
            Y1= 0               
       -154   Cm0  = 0,150   
                   -154 
                
                            
    OK         
                            
               .
                          
                  (  )        (  )  
         Long   Stability      STAB  
     OK         
               .


SSTAB  -  Side   Stability  -        
     Side   Stability           SSTAB 
                  
                     
           
              
              
                            
                      
     OK        
               .


LG  -  Landing  Gear  -   
    Landing  Gear        LG
                      
                         <Loading>  
                        
                        "0"   
        -154
                  
     OK  
              .


ABRS  -  Air  Brake  System  -        
      Air  Brake  System         ABRS
                
            -154
                  
     OK  
              .


BRS  -  Brake  System  -  C   
      Brake  System         BRS
                
            -154  (     141 )
                  
     OK  
              .


ARPT  -  Airport  -   
      ARPT          ARPT
       ICAO                   Airport  
       ICAO                     Airport  B
    OK                  
                        
                        
               .
           1500                          2000 
                 avia.world            
                   <Airport>                 Excel


  <Flight>  
=================================================================================================
         

         /   
                             
               
                           

                
-                           lbs 
-                  V=0   H=0                 
-      
-                                                                                 
-          %    
-                         
-                     
-                    
-                                                                   
-            ..     
             - 154

      
-               /       
-                  /       
-             /       
-                   
-                          
-                   
-            



  <Landing>  
=================================================================================================
         .
                
                  

L1 -                    
T1 -              L1                   (       )

L2 -                          "" 
T2 -              L2                   (     0     60  )

L3 -             "" 
T3 -              L3                  (     0     60  )

L4 -                   ""            "" 
T4 -              L4                  (     0     60  )

L5 -                "" 
T5 -              L5                  (     0     60  )

V23 -           L2    L3
V34 -           L3    L4                ""  
V45 -           L4    L5      

        < Vy >    (      0     10    /  )
                    <  H >     (      0     20    )

         /   
                             
               
                           

                
-                           lbs
-              "  "                           
-                                                                       
-                                                                                          
-                     
-                  ,                
-                     
-               
-            ..   
             - 154

      
-        L1 - L5
-         L              
-         L             
-            
-                     
-                
-              
-               



  <GWA>  
=================================================================================================
Geometric  Wing   Analyzer  -          
                    
                
                  ( points ) 

Point 1 -  
Point 2 - 
Point 3 - Ƹ
Point 4 - 
Point 5 - 
Point 6 - 
Point 7 - 
Point 8 - 

                         <GWA>
          > 
                      
                      <>        
               
                              
                      
                                
                                  
                         PUSH   POINTS 
                               FORWARD    PLAN  
                             
                                     
                                  
         -                        
                   1  5     2  6    3  7    4  8          
  1 - 2 - 3 - 4             
  5 - 6 - 7 - 8             
  1    5                  
  4    8                  
                     
                 ANALYSIS


 !
================================================================================================
              .
      (       FMC )               
              .
      !!!              !!!
                  !!!   

                          FMC
           Excel          FMC        
1 -             
2 -                  
3 -       OK       
4 -                

            
 -           <Flight>  
 -           <Landing> 
ND         <Cockpit>   
         Excel              


                   
              .
       ,          
mva1968@yandex.ru
  !
   

   
================================================================================================
. . , . . , . .   
          -154

.., ..  
    I.       

 ..,  ..  
    I         

 ..
, ,     

     
      

. . 
            

. . , . . 
    ,         
          2011

 ..   ..   ..
        
 

