Bleed system design technology for supersonic inlets
Author:
Affiliation:
1. Boeing Co., Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1972-1138
Reference7 articles.
1. of the SST Prototype Air Intake, report FAA-SS-72-50.
2. A procedure for combined viscous-inviscid analysis of supersonic inlet flow fields
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1. Aerothermal characteristics of bleed slot in hypersonic flows;Science China Physics, Mechanics & Astronomy;2015-09-05
2. Experimental Investigation of a Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Sweep-forward High- light and Bleed Slot in an Inverted “X”-type Layout;Chinese Journal of Aeronautics;2007-08
3. Supersonic-inlet boundary-layer bleed flow;AIAA Journal;1996-04
4. Shock-wave/boundary-layer interactions with bleed. II - Effect of slot location;Journal of Propulsion and Power;1995-11
5. Shock-wave/boundary-layer interactions with bleed. I - Effect of slot angle;Journal of Propulsion and Power;1995-11
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