Heat transfer and transition mechanism on a shock-tube wall
Author:
Affiliation:
1. U.S. Military Academy, West Point, New York
2. Rensselaer Polytechnic Institute, Troy, New York
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8813
Reference35 articles.
1. Boundary-Layer Transition and Heat Transfer in Shock Tubes
2. Use of the Shock Tube Wall Boundary Layer in Heat Transfer Studies
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