Matching of Auxiliary Inlets to Secondary-Air Requirements of Aircraft Ejector Exhaust Nozzles
Description:
Report presenting an analysis of the problems associated with matching secondary-air requirements of ejector exhaust nozzles and auxiliary inlets has been made for free-stream Mach numbers up to 2.0. The analysis indicated that inlets located in the free stream supply higher pressure recovery than ejectors generally require for optimum net internal thrust at Mach numbers above about 1.4. Net-thrust gains can be achieved by immersing the auxiliary inlet in a boundary layer where the inlet-moment…
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Date:
August 16, 1955
Creator:
Hearth, Donald P.; Englert, Gerald W. & Kowalski, Kenneth L.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department