Friction and heat-transfer effects on the nonsteady flow behind a detonation.

Publisher Website

1 November 1967

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

Vol. 5 (11), 2069-2071
https://doi.org/10.2514/3.4374

Abstract

No abstract available

This publication has 5 references indexed in Scilit:

Transfer behind detonations in H sub 2-O sub 2 mixtures.
AIAA Journal, 1966
Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactions
AIAA Journal, 1964
A numerical solution of unsteady flow problems
International Journal of Mechanical Sciences, 1964
Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic Flow
Journal of the Aerospace Sciences, 1961
THEORETICAL INVESTIGATION OF THE INFLUENCE OF VISCOUS FRICTION ON A PLANE WAVE OF FINITE MPLITUDE IN A COMPRESSIBLE FLUID
The Quarterly Journal of Mechanics and Applied Mathematics, 1956

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