Integral theory for supersonic turbulent base flows.
Author:
Affiliation:
1. California Institute of Technology, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4746
Reference44 articles.
1. Nash, J. F. "An Analysis of Two Dimensional Turbulent Base Flow Including the Effect of the Approaching Boundary Layer," Aero Rept. 1036,1962, National Physical Lab.
2. A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic Streams
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