Comparison of the unstart/restart processes of a two-dimensional twin-duct supersonic inlet induced by the plug throttling and thermal choking at the sideslip state

Author:

Li Teng-fei,Ding Run-han,Wang Wei-xing,Xie Wen-zhong

Funder

National Natural Science Foundation of China

Qinglan Project of Jiangsu Province of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

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4. Computational study on hysteretic inlet buzz characteristics under varying mass flow conditions;Hong;AIAA J.,2014

5. Numerical simulation of inlet buzz;Abedi;Aerosp. Sci. Technol.,2020

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