Search U.S. government technical reports digitized or harvested by TRAIL.
The effect of lip shape on a nose-inlet installation at Mach numbers from 0 to 1.5 and a method for optimizing engine-inlet combinations
An experimental investigation of the air-flow of a scoop-type normal-shock inlet
Fuselage side inlets : a study of some factors affecting their performance and a comparison with nose inlets
A study of a symmetrical, circular, internal, compression inlet