Browse TRAIL Inventories

Tests of a small-scale NACA submerged inlet at transonic Mach numbers

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

Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic 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

Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds


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