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by Theo G. Keith
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Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot
A. G. Powell
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
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
Charles J. Trefny
Noise suppression with high Mach number inlets
Edward Lumsdaine
Tests 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
Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
Michael A. Boles
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
Scott D. Holland
Simulated flight effects on noise characteristics of a fan inlet with high throat Mach number
Howard L. Wesoky
Numerical simulation of helicopter engine plume in forward flight
Arsenio C. B. Dimanlig
Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane
William G. Steenken
