Turbine separation control using pulsed vortex generator jets

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2000, Pages

  Bons, Jeffrey P ^a   Sondergaard, Rolf ^b   Rivir, Richard B ^b  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Control; Separation; Turbine.; VGJ

Indexed keywords

AIRCRAFT ENGINES; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; CONTROL; ENGINES; FLOW CONTROL; HEAT TRANSFER; LOCATION; REYNOLDS NUMBER; SEPARATION; SOLENOID VALVES; TURBINE COMPONENTS; TURBINES; TURBOMACHINE BLADES; VORTEX FLOW; VORTICITY;

BLADE SUCTION SURFACE; EXPERIMENTAL EVIDENCE; HIGH-ALTITUDE AIRCRAFTS; LINEAR TURBINE CASCADES; LOW PRESSURE TURBINE BLADE; STATIC PRESSURE DISTRIBUTIONS; TURBINE INLET TEMPERATURE; VGJ;

FIGHTER AIRCRAFT;

EID: 84881468164     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0262     Document Type: Conference Paper

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