Box 6
     Container 
  
Contains 87 Results:
Preliminary report on the combustion temperature and the exponent k of the adiabatic curve., 1940-01-19
     File  — Box: 6, Folder: 33/1
  
        Dates: 
      1940-01-19
    
  
    
  
The favorable expansion angle for Laval nozzles, 1940-02-05
     File  — Box: 6, Folder: 33/2
  
        Dates: 
      1940-02-05
    
  
    
  
The most favorable dimensioning of a Laval nozzle with a time-varying external pressure, 1940-04-08
     File  — Box: 6, Folder: 33/3
  
        Dates: 
      1940-04-08
    
  
    
  
Investigation of the influence of incomplete combustion with an excess of oxygen on the functioning of the furnaces developed by the Army Research Center, 1940-10-25
     File  — Box: 6, Folder: 33/6
  
        Dates: 
      1940-10-25
    
  
    
  
The thrust of 25 to furnaces with variable external pressure, 1941-01-29
     File  — Box: 6, Folder: 33/7
  
        Dates: 
      1941-01-29
    
  
    
  
