Flow and heat transfer measurements in a pseudo-shock region with surface cooling
Author:
Affiliation:
1. Jet Propulsion Lab., California Institute of Technology, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7279
Reference14 articles.
1. Structure of Shock Waves in Cylindrical Ducts
2. Wall Shear and Boundary-Layer Measurements in Shock Seperated Flow
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