Investigation of Segmented Bleed Model in Supersonic Turbulent Boundary Layer-Reference-Cited by-同舟云学术

Investigation of Segmented Bleed Model in Supersonic Turbulent Boundary Layer

Published:2011-01-04 Issue: Volume: Page:
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Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Manavasi Seshagopal¹,Morell A.¹,Hamed Awatef¹

Affiliation:

1. University of Cincinnati

Publisher

American Institute of Aeronautics and Astronautics

Link

Reference46 articles.

3. Willis,B.,Davis,B.,andHingst,W."FlowCoefficientBehaviorforBoundary-LayerBleedHolesandSlots,"AIAAPaper 95-0031,January1995.

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