Object 66/1 - 66/31
     Container 
  
Contains 30 Results:
Report No. 21 on the mechanics of the vertical ascent of an R-body in a vacuum with views of the conditions in the air-filled space, 1940-03-02
     File  — Object: 66/1 - 66/31, Folder: Arch 66/21
  
        Dates: 
      1940-03-02
    
  
    
  
Report No. 22 On the concept of entropy, 1940-02-27
     File  — Object: 66/1 - 66/31, Folder: Arch 66/22
  
        Dates: 
      1940-02-27
    
  
    
  
Report No. 23, Influence of the jet on the aerodynamic properties of the A5 power unit, 1940-03-12
     File  — Object: 66/1 - 66/31, Folder: Arch 66/23
  
        Dates: 
      1940-03-12
    
  
    
  
Report No. 24 The straight compression shock
     File  — Object: 66/1 - 66/31, Folder: Arch 66/24
  
        Dates: 
      1920 - 1970
    
  
    
  
Report No. 25 Spin stabilization of the A4 using air rudders, taking into account an asymmetric tail unit, 1940-04-09
     File  — Object: 66/1 - 66/31, Folder: Arch 66/25 (Copy)
  
        Dates: 
      1940-04-09
    
  
    
  
Airbrake report continued 05/15/39 - AA/FL No 8, 1940-07-19
     File  — Object: 66/1 - 66/31, Folder: Arch 66/26 (Copy)
  
        Dates: 
      1940-07-19
    
  
    
  
Three-component wind tunnel measurements on 15 cm DOV projectiles, 1940-07-17
     File  — Object: 66/1 - 66/31, Folder: Arch 66/27
  
        Dates: 
      1940-07-17
    
  
    
  
Preliminary report on measurements with the glider A4 V12/a, 1940-07-26
     File  — Object: 66/1 - 66/31, Folder: Arch 66/28
  
        Dates: 
      1940-07-26
    
  
    
  
On the question of attacking vibrations during the flight of an uncontrolled R-body, 1940-08-03
     File  — Object: 66/1 - 66/31, Folder: Arch 66/29 (Copy)
  
        Dates: 
      1940-08-03
    
  
    
  
The Prandtl-Busemann approximation method for following plane supersonic flows in graphic form, 1940-08-21
     File  — Object: 66/1 - 66/31, Folder: Arch 66/31
  
        Dates: 
      1940-08-21
    
  
    
  
