The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary Layer
Author:
Abstract
Publisher
Cambridge University Press (CUP)
Subject
General Engineering
Reference7 articles.
1. Stanbrook A. The surface oil flow technique used in high speed wind tunnels. RAE Tech. Note Aero. 2712, 1960.
2. Maskell E. C. Flow separation in three dimensions. RAE Report Aero. 2565, 1955.
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