Numerical Simulation of High-Speed Civil Transport Inlet Operability with Angle of Attack
Author:
Affiliation:
1. Rutgers University, Piscataway, New Jersey 08854
2. United Technologies Research Center, East Hartford, Connecticut 06180
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.503
Reference26 articles.
1. Results from computational analysis of a mixed compression supersonic inlet
2. PARC Code: Theory and Usage
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