Combustion properties of aluminum as ram-jet fuel
Description:
Report presenting an experimental investigation to determine the combustion properties of aluminum as a fuel for use in high-speed aircraft. The aluminum fuel was injected both in powder and wire form into 2-inch-diameter ramjet-type combustors. Results regarding operational problems, thrust, and combustion efficiency are provided.
Date:
March 28, 1951
Creator:
Branstetter, J. Robert; Lord, Albert M. & Gerstein, Melvin
Item Type:
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Partner:
UNT Libraries Government Documents Department