A boundary layer transition model

ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996

Volumn 1, Issue , 1996, Pages

  Johnson, Mark W ^a   Ercan, Ali H ^a  

^a UNIVERSITY OF LIVERPOOL   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; FRICTION; GAS TURBINES; TURBOMACHINE BLADES; TURBOMACHINERY; TURBULENCE; TURBULENT FLOW;

BOUNDARY LAYER TRANSITIONS; FREESTREAM TURBULENCE; FREQUENCY SPECTRA; INTEGRAL TECHNIQUES; NEAR WALL VELOCITY; SKIN FRICTION COEFFICIENT; VELOCITY FLUCTUATIONS; ZERO PRESSURE GRADIENT;

ATMOSPHERIC THERMODYNAMICS;

EID: 84923923877     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/96-GT-444     Document Type: Conference Paper

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