Laminar heat transfer to a two-dimensional backward facing step from the high-enthalpy supersonic flow in the shock tube-Reference-Cited by-同舟云学术

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Laminar heat transfer to a two-dimensional backward facing step from the high-enthalpy supersonic flow in the shock tube

Published:1964-02 Issue:2 Volume:2 Page:251-255
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

ROM JOSEF¹,SEGINER ARNAN¹

Affiliation:

1. Technion-Israel Institute of Technology, Haifa, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.2295

Reference10 articles.

1. October 1956;Chapman D R

2. Some Experiments on Hypersonic Separated Flows

3. September 1961;Chung P M

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