Active flow separation control of a stator vane using surface injection in a multistage compressor experiment

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 6 B, Issue , 2003, Pages 1039-1050

  Culley, Dennis E ^a   Prahst, Patricia S ^b   Bright, Michelle M ^a   Strazisar, Anthony J ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

^b AP Solutions Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL COMPRESSORS; PRESSURE LOSS;

ALGORITHMS; CLOSED LOOP CONTROL SYSTEMS; FLOW CONTROL; FLUIDIC DEVICES; JETS; OSCILLATIONS; RELIABILITY; STATORS;

COMPRESSORS;

EID: 0348217796     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38863     Document Type: Conference Paper

References (14)

1. Amitay, M., Kibens, V., Parekh, D., and Glezer A., 1999, "The Dynamics of Flow Reattachment over a Thick Airfoil Controlled by Synthetic Jet Actuators," AIAA Paper No. 99-1001.
2. Seifert, A., Bachar, T., Koss, D., Shepshelovich, M., and Wygnanski, I., 1993, "Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation," AIAA J., 31, No. 11, pp. 2052-2060.
3. McManus, K., Legner, H., and Davis, S., 1994, "Pulsed Vortex Generator Jets for Active Control of Flow Separation," AIAA Paper No. 94-2218.
4. Amitay, M., and Glezer, A., 1999, "Aerodynamic Flow Control of a Thick Airfoil Using Synthetic Jet Actuators," ASME/JSME Paper FEDSM99-6922.
5. Carter, C., Guillot, S., Ng, W., and Copenhaver, W., 2001, "Aerodynamic Performance of a High-Turning Compressor Stator with Flow Control," AIAA Paper 2001-3973.
6. Stitzel, S., 2002, "Integrated Ejector Pump Flow Control for Low Pressure Turbine," NASA Phase I SBIR Final Report, NASA-LPT-FR01.
7. Bons, J., Sondergaard, R., and Rivir, R., 2000, "Turbine Separation Control Using Pulsed Vortex Generator Jets," ASME J. Turbomachinery, 123, pp. 198-206.
8. Bons, J., Sondergaard, R., and Rivir, R., 2002, "The Fluid Dynamics of LPT Blade Separation Control Using Pulsed Jets," ASME J. of Turbomachinery, 124, pp. 77-85.
9. Wasserbauer, C.A., Weaver, H.F., and Senyitko, R.G., 1995, "NASA Low Speed Compressor for Fundamental Research," NASA TM4635.
10. Wisler, D.C., 1977, "Core Compressor Exit Stage Study: Volume I - Blade Design," NASA CR135391.
11. Wellborn, S., and Okiishi, T., 1999, "The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance," ASME J. of Turbomachinery, 121, pp. 486-498.
12. Nishri, B., and Wygnanski, I., 1998, "Effects of Periodic Excitation on Turbulent Flow Separation from a Flap," AIAA Journal, 36, No. 4, pp. 547-556.
13. Brocher, E., 1961, "The Jet-Flap Compressor Cascade," ASME Journal of Basic Engineering, p. 401.
14. Kim, B., Williams, D., Emo, S., and Acharya, M., 2002, "Large Amplitude Pneumatic Oscillator for Pulsed-Blowing Actuators", AIAA Paper 2002-2704.