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