Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
7 results returnedSearch results
- 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