Effects of high-speed tunnel noise on laminar-turbulent transition

Journal of Spacecraft and Rockets

Volumn 38, Issue 3, 2001, Pages 323-333

  Schneider, S P ^a  

^a PURDUE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPUTER SIMULATION; HYPERSONIC FLOW; LAMINAR FLOW; REYNOLDS NUMBER; SUPERSONIC FLOW; TRANSITION FLOW; TURBULENT FLOW; WIND TUNNELS;

LAMINAR-TURBULENT TRANSITIONS; TUNNEL NOISE;

ACOUSTIC NOISE;

EID: 0035332207     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3705     Document Type: Conference Paper

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