Numerical Investigations of Aeroheating for Missile Slots-Reference-Cited by-同舟云学术

Numerical Investigations of Aeroheating for Missile Slots

Published:2016-01 Issue:1 Volume:29 Page:04015028
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yang Kai¹,Bai Yuguang²,Zhu Qianghua²,Gao Xiaowei³

Affiliation:

1. Associate Professor, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian Univ. of Technology, Dalian 116023, China (corresponding author).

2. Lecturer, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian Univ. of Technology, Dalian 116023, China.

3. Professor, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian Univ. of Technology, Dalian 116023, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000511

Reference11 articles.

1. Hypersonic and High-Temperature Gas Dynamics, Second Edition

2. Numerical/Experimental Correlation of a Plasma Wind Tunnel Test on a UHTC-Made Nose Cap of a Reentry Vehicle

3. Cleary J. W. (1969). “Effects of angle of attack and bluntness on laminar heating-rate distributions of a 15° cone at a Mach number of 10.6.” Vol. 5450 National Aeronautics and Space Administration.

4. Engineering relations for friction and heat transfer to surface in high velocity flow;Eckert E. R. G.;J. Aeronaut. Sci.,1955

5. Theory of stagnation point heat transfer in dissociated air;Fay J. A.;J. Aeronau. Sci.,1958

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