Variable Geometry for Supersonic Mixed-Compression Inlets
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58659
Reference8 articles.
1. 3;Supersonic Transport Development Program,1984
2. Possibilities for Improved Supersonic Inlet Performance
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