Displacement thickness for boundary layers with surface mass transfer.
Author:
Affiliation:
1. Avco Corporation, Wilmington, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3641
Reference8 articles.
1. EFFECTIVE DISPLACEMENT THICKNESS FOR BOUNDARY LAYERS WITH SURFACE MASS TRANSFER
2. BLOWING EFFECTS ON PRESSURE INTERACTION ASSOCIATED WITH CONES
3. Transverse Curvature Effects in Axisymmetric Hypersonic Boundary Layers
4. SECOND-ORDER COMPRESSIBLE BOUNDARY LAYER THEORY WITH APPLICATION TO BLUNT BODIES IN HYPERSONIC FLOW
5. The laminar compressible boundary-layer in the stagnation-point region of an axisymmetric blunt body including the second-order effect of vorticity interaction
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1. Systematic Comparison of Mathematically Simple Turbulence Models for Three-Dimensional Boundary Layers;AIAA Journal;1993-06
2. Analysis of boundary layers on perforated walls of transonic wind tunnels;Journal of Aircraft;1981-06
3. Die Verdrängungsdicke bei Grenzschichten höherer Ordnung;ZAMM - Zeitschrift für Angewandte Mathematik und Mechanik;1974
4. COMMENT ON "FINITE ELEMENTS FOR AXISYMMETRIC SOLIDS UNDER ARBITRARY LOADINGS WITH NODES OF ORIGIN';AIAA Journal;1973-09
5. Reply by Author to G.R. Inger;AIAA Journal;1973-09
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