Characteristic analysis of unstart/restart of hypersonic inlets caused by variations of attack angle of freestream

Hangkong Dongli Xuebao/Journal of Aerospace Power

Volumn 23, Issue 5, 2008, Pages 816-821

  Chang, Jun Tao ^a   Yu, Da Ren ^a   Bao, Wen ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Aerospace propulsion system; Hypersonic inlets; Numerical simulation; Restart; Unstart

Indexed keywords

FLOW FIELDS; HYDRODYNAMICS; MACH NUMBER;

AEROSPACE PROPULSION SYSTEM; HYPERSONIC INLETS; NUMERICAL SIMULATION; RESTART; UNSTART;

ANGLE OF ATTACK;

EID: 45449100200     PISSN: 10008055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (14)

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