Numerical Investigation of Sweep Angle Effect on the Supersonic Flows through Corners-Reference-Cited by-同舟云学术

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Numerical Investigation of Sweep Angle Effect on the Supersonic Flows through Corners

Published:2017-07 Issue:4 Volume:30 Page:04017005
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Kharati-Koopaee Masoud¹,Mohammadpour-Shoorbakhloo Mojtaba²

Affiliation:

1. Assistant Professor, Dept. of Mechanical and Aerospace Engineering, Shiraz Univ. of Technology, 7155713876 Shiraz, Iran (corresponding author).

2. M.Sc. Student, Dept. of Mechanical and Aerospace Engineering, Shiraz Univ. of Technology, 7155713876 Shiraz, Iran.

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.1943-5525.0000715

Reference26 articles.

1. Fluent version 6.3.26 [Computer software]. Fluent Inc. Lebanon NH.

2. Gambit version 2.4 [Computer software]. Fluent Inc. Lebanon NH.

3. Supersonic interference flow along the corner of intersecting wedges.

4. Eagle W. E. and Driscoll J. F. (2011). “Experimental investigation of corner flows in rectangular supersonic inlets with 3D shock-boundary layer effects.” 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition American Institute of Aeronautics and Astronautics Reston VA.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Coupled investigation on drag reduction and thermal protection mechanism induced by a novel combinational spike and multi-jet strategy in hypersonic flows;International Journal of Heat and Mass Transfer;2019-03

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