An experimental investigation of transition as applied to low pressure turbine suction surface flows

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1997, Pages

  Qiu, Songgang ^a   Simon, Terrence W ^a  

^a University of Minnesota   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; BOUNDARY LAYERS; FLOW SEPARATION; GAS TURBINES; REYNOLDS NUMBER; SHEAR FLOW; SIZE SEPARATION; TRANSITION FLOW; WALL FLOW;

ENHANCED TRANSPORTS; EXPERIMENTAL INVESTIGATIONS; FREESTREAM TURBULENCE; HOT-WIRE TECHNIQUES; INTERMITTENCY DISTRIBUTIONS; LOW-PRESSURE TURBINES; SEPARATED SHEAR LAYERS; SURFACE STATIC PRESSURE;

FIGHTER AIRCRAFT;

EID: 84973642045     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-455     Document Type: Conference Paper

References (19)

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