General Reynolds Analogy for Blunt-Nosed Bodies in Hypersonic Flows-Reference-Cited by-同舟云学术

General Reynolds Analogy for Blunt-Nosed Bodies in Hypersonic Flows

Published:2015-08 Issue:8 Volume:53 Page:2410-2416
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Chen Xing-Xing¹,Wang Zhi-Hui¹,Yu Yong-Liang¹

Affiliation:

1. School of Physical Sciences, University of the Chinese Academy of Sciences, 100049 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053962

Reference19 articles.

1. Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds

2. Theory of Stagnation Point Heat Transfer in Dissociated Air

3. Laminar Heat Transfer Around Blunt Bodies in Dissociated Air

4. Laminar boundary layer on a sphere in hypersonic flow of equilibrium dissociating air

5. BeckwithI. E.GallagherJ. J. “Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers,” NASA TR-R104, May 1962.

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