Altitude-Test-Chamber Investigation of Performance of a 28-Inch Ram-Jet Engine 4: Effect of Inlet-Air Temperature, Combustion-Chamber-Inlet Mach Number, and Fuel Volatility on Combustion Performance
Description:
Report presenting testing of the effects of the following variables on combustion performance are determined: inlet-air temperature, combustion-chamber-inlet Mach number and pressure, and fuel density and volatility.
Date:
July 27, 1951
Creator:
Kahn, Robert W.; Nakanishi, Shigeo & Harp, James L., Jr.
Item Type:
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Partner:
UNT Libraries Government Documents Department