Rapid prediction method for wall heat flux within gap induced by supersonic flow based on log-linear distribution law

Author:

Zha Zhang-MingORCID,Li Dong,Xie Xiang-Qian,Chen Xin,Du Shen,He Ya-Ling

Publisher

Elsevier BV

Reference37 articles.

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3. Combustion enhancement subjected to the inlet distortion in a cavity-based supersonic combustor;Li;Aerosp. Sci. Technol.,2023

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5. Heat transfer to steps and cavities in hypersonic turbulent flow;Nestler;AIAA J.,1969

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