Variations of the shock and secondary flow structure in a transonic compressor cascade with outlet back pressure

The effects of back pressure on the transonic cascade operating state are crucial and can determine the structure of internal shock waves and secondary flows. In this paper, numerical methods validated by experiments were employed to investigate the evolution mechanisms of the inlet flow field, shoc...

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Veröffentlicht in:	Physics of fluids (1994) 2024-06, Vol.36 (6)
Hauptverfasser:	Meng Fanjie, Tang, Jie, Li Jingyin, Gong Chaoxuan, Guo Penghua
Format:	Artikel
Sprache:	eng
Schlagworte:	Boundary layers Cascade flow Fluid flow Inlet flow Numerical methods Pressure effects Pressure ratio Secondary flow Shock waves Static pressure Three dimensional flow Transonic compressors Two dimensional flow
Online-Zugang:	Volltext
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