Displacement thickness for boundary layers with surface mass transfer.

Publisher Website

1 June 1966

journal article
Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal

Vol. 4 (6), 1142-1144
https://doi.org/10.2514/3.3641

Abstract

No abstract available

This publication has 6 references indexed in Scilit:

Transverse Curvature Effects in Axisymmetric Hypersonic Boundary Layers
AIAA Journal, 1964
The laminar compressible boundary-layer in the stagnation-point region of an axisymmetric blunt body including the second-order effect of vorticity interaction
International Journal of Heat and Mass Transfer, 1964
BLOWING EFFECTS ON PRESSURE INTERACTION ASSOCIATED WITH CONES
AIAA Journal, 1963
EFFECTIVE DISPLACEMENT THICKNESS FOR BOUNDARY LAYERS WITH SURFACE MASS TRANSFER
AIAA Journal, 1963
SECOND-ORDER COMPRESSIBLE BOUNDARY LAYER THEORY WITH APPLICATION TO BLUNT BODIES IN HYPERSONIC FLOW
Published by Elsevier ,1962
On displacement thickness
Journal of Fluid Mechanics, 1958

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