A procedure for solving the compressible interacting boundary-layer equations for subsonic and supersonic flows-Reference-Cited by-同舟云学术

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A procedure for solving the compressible interacting boundary-layer equations for subsonic and supersonic flows

Published:1984-06-25 Issue: Volume: Page:
ISSN:
Container-title:17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

DAVIS R.¹

Affiliation:

1. Cincinnati, University, Cincinnati, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1614

Reference13 articles.

1. Progress on Interacting Boundary-Layer Computations at High Reynolds Number

2. StewartSOn, K. "Multistructured Boundary Layers on Flat Plates and Related Bodies,'' Advances in Applied Mechanics, Academic Press, Inc., Vol. 14,1974, pp.145-239.

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1. Supersonic Breakaway Separation Past an Adiabatic Wavy Wall;AIAA Journal;1998-04

2. Boundary-layer tripping by a roughness element;Journal of Propulsion and Power;1996-07

3. The critical allowable height of a backward-facing step;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

4. Transition in flow over heat‐transfer strips;Physics of Fluids;1995-09

5. Compressible boundary-layer tripping by blowing;Fluid Dynamics Conference;1995-06-19

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