Search U.S. government technical reports digitized or harvested by TRAIL.
Air-flow surveys in the vicinity of representative NACA 1-series cowlings
Tests of a small-scale NACA submerged inlet at transonic Mach numbers
A survey of methods for turbojet thrust measurement applicable to flight installation
Preliminary attempts at isothermal compression of a supersonic air stream
Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds
A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05
An inlet design concept to reduce flow distortion at angle of attack