Comparison of flight performance of AN-F-58 and AN-F-32 fuels in J35 turbojet engine
Description:
Report presenting a flight investigation to determine the comparative performance of AN-F-58 and AN-F-32 fuels in a 4000-pound-thrust turbojet engine. The fuels were equivalent over the range of conditions investigated. Results regarding corrected net thrust, corrected jet-fuel consumption, variation of corrected tail-pipe temperature, combustor blow-out speeds, and visual observations of the jet exhaust are provided.
Date:
April 7, 1949
Creator:
Acker, Loren W. & Kleinknecht, Kenneth S.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department