Effects of compressibility and turbulence level on bypass transition

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1998, Pages

  Schook, R ^a   De Lange, H C ^a   Van Steenhoven, A A ^a  

^a EINDHOVEN UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMPRESSIBILITY; GAS TURBINES; HEAT TRANSFER; MACH NUMBER; REYNOLDS NUMBER; TURBOMACHINERY; TURBULENCE;

BOUNDARY LAYER TRANSITIONS; BYPASS TRANSITION; ENERGY SPECTRA; HEAT TRANSFER MEASUREMENTS; INERTIAL RANGES; TRANSITION CURVES; TRANSITION MODEL; TURBULENCE LEVEL;

ATMOSPHERIC THERMODYNAMICS;

EID: 84971500290     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/98-GT-286     Document Type: Conference Paper

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