Flat Plate Turbulent Boundary Layers Subject to Large Pressure Fluctuations
Author:
Affiliation:
1. The Queen 's University of Belfast, Belfast, N. Ireland
2. Royal Aircraft Establishment, Bedford, England
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61073
Reference10 articles.
1. Inviscid Flowfield Calculations for Re-entry Vehicles with Control Surfaces
2. Aerodynamic comparison of a conical and biconic reentry vehicle
3. ANALYSIS OF THE ANGULAR MOTION OF MISSILES.
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1. Effects of compressibility and free-stream turbulence on boundary layer transition in high-subsonic and transonic flows;14th Aerodynamic Testing Conference;1986-03-05
2. Freestream turbulence effects on attached subsonic turbulent boundary layers;AIAA Journal;1983-04
3. Algorithm for rapid integration of turbulence model equations on parabolic regions;AIAA Journal;1981-02
4. Pressure fluctuations in transonic shock-induced separation;AIAA Journal;1981-02
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