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Report presenting values of zero angle-of-attack performance of a double-cone inlet with and without a shroud through a range of mass-flow ratios and Mach numbers. Maximum propulsive thrust was… (More)
NACA RM E531,28bNATIONAL ADVISORY COMMITTEE FOR AERONAUTICSRESEARCH MEMORANDUM INTERNAL PERFORMANCE AT MACH NUMBERS TO 2.0 OF TWO AUXILIARY INLETS IMMERSED IN FUSELAGE BOUNDARY LAYER By Donald B.… (More)
An investigation of the jet-spreading characteristics of a 16 inch ram-jet engine was conducted in the 8 by 6 foot supersonic tunnel at a Mach number of 2.0; both a converging nozzle having a… (More)
"An investigation of the performance of a 16-inch ram jet engine having a single oblique-shock all-external compression inlet designed for a flight Mach number of 1.8, was conducted in the NACA Lewis… (More)
Report presenting an investigation to determine the effect of circumstantial inlet location on the performance of twin half-conical scoop-type inlets with and without boundary-layer removal at… (More)