Direct numerical simulation of hypersonic boundary-layer transition over blunt leading edges, Part II: Receptivity to sound

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Zhong, Xiaolin ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; DIRECT NUMERICAL SIMULATION; HYPERSONIC FLOW; LINEAR STABILITY ANALYSIS; NAVIER STOKES EQUATIONS; NUMERICAL MODELS; PLASMA SHOCK WAVES; STABILITY;

ACOUSTIC DISTURBANCES; BLUNT LEADING EDGES; BOUNDARY LAYER INSTABILITY; ENVIRONMENTAL DISTURBANCES; EXTERNAL DISTURBANCES; INSTABILITY WAVES; MODE INSTABILITIES; NUMERICAL RESULTS;

HYPERSONIC BOUNDARY LAYERS;

EID: 84983158139     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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