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4 results returnedPreliminary attempts at isothermal compression of a supersonic air stream
An analog study of a shock-position diffuser control on a supersonic turbojet engine
An inlet design concept to reduce flow distortion at angle of attack
Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet
Published Year
Subject
- Charts, diagrams, etc (4)
- Diffusers (4) *
- Air flow (2)
- Jet engines--Air intakes (2)
- Aerodynamics, Supersonic (1)
- Air ducts (1)
- Airplanes--Motors--Cowlings (1)
- Airplanes--Nacelles (1)
- Airplanes--Turbojet engines (1)
- Airplanes--Turbojet engines--Control systems (1)
- Angle of attack (Aerodynamics) (1)
- Pressure (1)
- Pressure--Measurement (1)
Author
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