Flat-Faced Leading-Edge Effects in Low-Density Hypersonic Wedge Flow
Author:
Affiliation:
1. National Institute for Space Research, SP 12630-000 Cachoeira Paulista, Brazil
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.4907
Reference24 articles.
1. Aerodynamic Problems of Manned Space Vehicles
2. Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic Flow
3. Surface measurements on sharp flat plates and wedges in low-density hypersonic flow.
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1. Bluntness Effects on Lift-to-Drag Ratio of Leading Edges for Hypersonic Waverider Configurations;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24
2. Heat transfer—A review of 2005 literature;International Journal of Heat and Mass Transfer;2010-10
3. Physical and Numerical Aspects of Simulating Rarefied Hypersonic Wedge Flow;Journal of Spacecraft and Rockets;2010-05
4. Bluntness Impact on Lift-to-Drag Ratio of Hypersonic Wedge Flow;Journal of Spacecraft and Rockets;2009-03
5. Leading Edge Thickness Impact on Drag and Lift in Hypersonic Wedge Flow;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08
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