Bluntness Impact on Lift-to-Drag Ratio of Hypersonic Wedge Flow
Author:
Affiliation:
1. National Institute for Space Research, 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/10.2514/1.41387
Reference26 articles.
1. Aerodynamic Problems of Manned Space Vehicles
2. Flat-Faced Leading-Edge Effects in Low-Density Hypersonic Wedge Flow
3. Effects of compressibility on aerodynamic surface quantities over low-density hypersonic wedge flow
4. Experimental Results on a Mach 14 Waverider with Blunt Leading Edges
5. Power Law Shapes for Leading-Edge Blunting with Minimal Shock Standoff
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