Simple Technique for Predicting Type 11 and IV Shock Interference
Author:
Affiliation:
1. Sandia Laboratories, Livermore, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49435
Reference8 articles.
1. ANOMALOUS HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON BLUNT BODIES AT HYPERSONIC SPEEDS IN THE PRESENCE OF AN IMPINGING SHOCK.
2. Shock Interference Bell Aerospace, Heating in Hypersonic Flows
3. A Graphical Method for the Investigation of Shock Interference Phenomena
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