Supersonic-inlet boundary-layer bleed flow
Author:
Affiliation:
1. NYMA, Inc., Brook Park, Ohio 44142
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13140
Reference25 articles.
1. Modeling supersonic inlet boundary-layer bleed roughness
2. Calculation of incompressible rough-wall boundary-layer flows
3. Some design considerations for supersonic cruise mixed compression inlets
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