Hysteresis of oscillatory airflow in a supersonic intake model

Author:

Kuzmin AlexanderORCID

Funder

Saint Petersburg State University

Publisher

Springer Science and Business Media LLC

Reference19 articles.

1. Shedon J (1999) Intake aerodynamics. Blackwell Publishing Ltd., London

2. Panchal D, Chhayani D (2021) Review paper on the unstarting of the supersonic air intake. Int J Eng Res Technol 10(12). https://www.ijert.org/review-paper-on-the-unstarting-of-the-supersonic-air-intake

3. Kusunose K, Matsushima K, Maruyama D (2011) Supersonic biplane—a review. Prog Aerosp Sci 47:53–87. https://doi.org/10.1016/j.paerosci.2010.09.003

4. Yamashita H, Kuratani N, Yonezawa M, Ogawa T, Nagai H, Asai K, Obayashi S (2013) Wind tunnel testing on start/unstart characteristics of finite supersonic biplane wing. Int J Aerosp Eng Hindawi. https://doi.org/10.1155/2013/231434. (Article 231434)

5. Guo S, Wang Z, Zhao Y (2014) The flow hysteresis in the supersonic curved channel. J Natl Univ Defense Technol 36(4):10–14

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