Aerothermodynamic Performance Analysis of Hypersonic Flow on Power Law Leading Edges
Author:
Affiliation:
1. National Institute for Space Research, 12630-000 Cachoeira Paulista-SP, Brazil
2. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.9550
Reference20 articles.
1. Aerodynamic Problems of Manned Space Vehicles
2. Experimental Results on a Mach 14 Waverider with Blunt Leading Edges
3. Aerodynamically blunt and sharp bodies
4. Power-Law Shaped Leading Edges in Rarefied Hypersonic Flow
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