Effect of noise on roughness-induced boundary-layer transition for scramjet inlet

Journal of Spacecraft and Rockets

Volumn 38, Issue 5, 2001, Pages 692-698

  Ito, Takeshi ^a,c   Randall, Laura A ^b   Schneider, Steven P ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b PURDUE UNIVERSITY   (United States)

^c Fluid Science Research Center   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

INTAKE SYSTEMS; REYNOLDS NUMBER; SPACE RESEARCH; SUPERSONIC AERODYNAMICS; TRANSITION FLOW; WIND TUNNELS;

BOUNDARY LAYER TRANSITIONS; SCRAMJET-INLET MODEL; SURFACE HOT-FILM MEASUREMENTS;

BOUNDARY LAYERS;

EID: 0035438997     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3754     Document Type: Article

References (22)

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