Passive control applied to Prandtl–Meyer expansion flow with homogeneous condensation
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
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2. L. Bahi, J.M. Ross, H.T. Nagamatsu, Passive shock wave/boundary layer control for transonic airfoil drag reduction, AIAA Paper-83-0137, 1983
3. B.S. Baldwin, H. Lomax, Thin layer approximation and algebraic model for separated turbulent flows, AIAA paper 78-257, 1978
4. Prandtl–Meyer flows with homogeneous condensation. Part 1, Subcritical flows;Delale;J. Fluid Mech.,1998
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1. Numerical investigation of homogeneous condensation in Prandtl–Meyer expansion flows;Shock Waves;2016-06-29
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