Analysis of hypersonic compression ramp laminar flows under sharp leading edge conditions-Reference-Cited by-同舟云学术

Analysis of hypersonic compression ramp laminar flows under sharp leading edge conditions

Published:2001-06 Issue:4 Volume:5 Page:257-271
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Marini Marco

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference20 articles.

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2. Temperature and velocity profiles in the compressible laminar boundary layer with arbitrary distribution of surface temperature;Chapman;J. Aerosp. Sci.,1949

3. Investigation of Separated Flows in Supersonic and Subsonic Streams with Emphasis on the Effect of Transition;Chapman,1957

4. Shock Interference Phenomena in Hypersonic Flows, The Third Joint Europe/US Short Course in Hypersonics;Délery,1990

5. Görtler instability of hypersonic boundary layer;De Luca;Exp. Fluids,1993

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