Some observations on reduction of turbulent boundary-layer heat transfer in nozzles.
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3885
Reference15 articles.
1. Hypersonic boundary-layer transition data for a cold-wall slender cone
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