Mechanisms of Hysteresis in the Acceleration and Deceleration Processes of Hypersonic Inlets-Reference-Cited by-同舟云学术

Mechanisms of Hysteresis in the Acceleration and Deceleration Processes of Hypersonic Inlets

Published:2023-05 Issue:3 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yang Shu-Zi¹,Liao Kai²,Xie Wen-Zhong³^ORCID,Yue Yan-Jun⁴,Yang Lin-Lin⁵,Guo Shengmin⁶

Affiliation:

1. Ph.D. Candidate, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, People’s Republic of China.

2. Assistant Engineer, Sichuan Gas Turbine Research Establishment, Aero Engine Corporation of China (AECC), Chengdu 610500, People’s Republic of China.

3. Professor, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, People’s Republic of China (corresponding author). ORCID: .

4. Engineer, Shanghai Institute of Mechanical and Electrical Engineering, Shanghai 201109, People’s Republic of China.

5. Postgraduate, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, People’s Republic of China.

6. Professor, Dept. of Mechanical Engineering, Louisiana State Univ., Baton Rouge, LA 70803.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4645

Reference33 articles.

1. Anderson, J. D. 2002. Computational fluid dynamics: The basics with applications. New York: McGraw-Hill.

2. Effects of boundary-layers bleeding on unstart/restart characteristics of hypersonic inlets

3. Edwards C. W. Small J. Weidner and P. Johnston. 1975. “Studies of scramjet/airframe integration techniques for hypersonic aircraft.” In Proc. 13th Aerospace Sciences Meeting. Reston VA: American Institute of Aeronautics and Astronautics.

4. Falempin F. E. Wendling M. Goldfeld and A. Starov. 2006. “Experimental investigation of starting process for a variable geometry air inlet operating from Mach 2 to Mach 8.” In Proc. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conf. & Exhibit. Reston VA: American Institute of Aeronautics and Astronautics.

5. Harvey, E. 2011. Shock wave-boundary-layer interaction. Cambridge, UK: Cambridge University Press.

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