The influence of acceleration on laminar similar boundary layers
Author:
Affiliation:
1. Ministry of Defense, Haifa, Israel
2. Technion—Israel Institute of Technology, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9112
Reference12 articles.
1. Acceleration and cooling effects in laminar boundary layers - Subsonic, transonic, and supersonic speeds
2. Compressible laminar boundary layers with large acceleration and cooling
3. 4Forbrich, C. A. "Improved Solutions to the Falkner Skan Boundary Layer Equation,*' AIAA Journal, Vol.9, Sept. 1982, pp.1306-1307.
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