Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot

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