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An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2
Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing
Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8
Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8
An inlet design concept to reduce flow distortion at angle of attack
Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet
Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination