Changes in heat transfer from turbulent boundary layers interacting with shock waves and expansion waves
Author:
Affiliation:
1. Jet Propulsion Laboratory, Pasadena, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6004
Reference12 articles.
1. THERMAL EFFECTS OF SHOCKWAVE TURBULENT BOUNDARY LAYER INTERACTION AT MACH NUMBERS 3 AND 5
2. Flow phenomena and convective heat transfer in a conical supersonic nozzle.
3. Laminarization of a Turbulent Boundary Layer in Nozzle Flow—Boundary Layer and Heat Transfer Measurements With Wall Cooling
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