Browse TRAIL Inventories

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


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