A study of several typical air inductions systems for modern aircraft indicate that flow distortions of about-pipe-flow magnitudes can be expected at near-optimum inlet-engine matched air-flow conditions and at small angles of attacks. These distortions may be seriously increased by operation at large angles of attack or yaw, or by supercritical operation of the inlets.
Factors Controlling Air-Inlet Flow Distortions
1956
16 pages
Report
No indication
English
Astronautics , Aircrafts , Mach number , Air flow , Boundary layer , Flow rate , Flow separation , Pipe flow , Airplanes , Flow , Bleed systems , Compressors , Engines , Induction systems , Boundaries , Diffusers , Distortion , Layers , Aeronautics , Free stream , Fuselages
Factors Controlling Air-inlet Flow Distortions
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