Experimental and numerical analysis of laminar flow control at Mach 1.4
Author:
Affiliation:
1. National Aerospace Lab., Mitaka, Japan
2. Kawasaki Heavy Industries, Ltd., Gifu, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-3655
Reference14 articles.
1. Mack, L.M. "Boundary-Layer Linear Stability Theory0022, Special Course on Stability and Transition of Laminar Flow, AGARD Rep. No.709, 3-l-81, 1984.
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