Flight Investigation of a Full-Scale Aircraft Ejector with Various Spacing Ratios and Correlation with Small-Scale Tests
Description:
Memorandum presenting a flight investigation to determine the thrust and pumping characteristics of a family of aircraft exhaust ejectors. Information was obtained on the variation of these characteristics with changes in engine power, flight Mach number, and ejector spacing ratio, and these results were compared to small-scale tests. Results were also obtained showing how a swinging survey probe can be used as a device for calibrating a tail-pipe pressure probe for the measurement of thrust an…
more
Date:
August 26, 1958
Creator:
Havill, C. Dewey & Wingrove, Rodney C.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department