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Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot
A. G. Powell1985
Género: Air intakes
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Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet
Bobby W. Sanders
1980
AñadirLow-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
Charles J. Trefny
1986
AñadirTests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [sic, i.e. 2.0]
M. C. Neale
1967
AñadirTheoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
Michael A. Boles
1978
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