Oscillatory flows of rectangular hypersonic inlet unstart caused by downstream mass-flow choking

Journal of Propulsion and Power

Volumn 25, Issue 1, 2009, Pages 138-147

  Tan, Hui Jun ^a,c   Sun, Shu ^a,d   Yin, Zhi Long ^b,e  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

^b HONGDU Aviation Industry Group   (China)

^c Jiangsu Province Key Laboratory of Aerospace Power System   (China)

^d College of Civil Aviation ^*

^e 660 Institute

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE PROPAGATION; ACOUSTIC WAVES; FEEDBACK; HYPERSONIC FLOW;

FREESTREAM MACH NUMBER; OSCILLATION FREQUENCY; OSCILLATION MECHANISM; OSCILLATORY FLOWS; SEPARATION BUBBLE; SUPERSONIC INLETS; SURFACE PRESSURE FLUCTUATIONS; UPSTREAM PROPAGATION;

HYPERSONIC INLETS;

EID: 63649097066     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.37914     Document Type: Article

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