Unsteady aerodynamics in transonic compressor rotor blade passages

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Minkiewicz, Greg ^a   Russler, Patrick ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b BATTELLE MEMORIAL INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; ENGINES; FREQUENCY DOMAIN ANALYSIS; PROPULSION; TRANSONIC AERODYNAMICS; TRANSONIC FLOW;

ENSEMBLE-AVERAGING TECHNIQUES; SHOCK BOUNDARY-LAYER INTERACTIONS; SPECTRAL DECOMPOSITION; TIME- AND FREQUENCY-DOMAIN ANALYSIS; TRANSIENT BEHAVIOR; TRANSONIC COMPRESSOR; TRANSONIC COMPRESSOR ROTOR; UNSTEADY AERODYNAMICS;

TURBOMACHINE BLADES;

EID: 84963805793     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Rabe, D. C., Boles, A., Russler, P. M., "Influence of Inlet Distortion on Transonic Compressor Blade Loading" AIAA 95-2461
2. Cybyk, B. Z, Rabe, D. C., Russler, P. M. and Hah, C., "Characterization of the First-Stage Rotor in a Two Stage Transonic Compressor" AIAA 95-2460
3. Russler, P. M., Rabe, D. C., Cybyk, B. Z. and Hah, C., 1995, "Tip Flow Fields in a Low Aspect Ratio Transonic Compressor" ASME Paper No. 95-GT-089.
4. Manwaring, S.R., Rabe, D.C., Lorence, C.B., and Wadia, A.R., "Inlet Distortion Generated Forced Response of a Low Aspect Ratio Transonic Fan" ASME Paper No. 96-GT-376
5. Hah, C., Rabe, D. C., Sullivan, T. J., Wadia, A. R., "Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor" ASME Paper 96-GT- 547
6. Wennerstrom, A. J., "Experimental Study of a High- Throughflow Transonic Axial Compressor Stage" ASME Journal of Engineering For Gas Turbines and Power, Vol. 106, July 1984.
7. Bendat Julius S., Piersol Allan G., Engineering Applications of Correlation and Spectral Analysis. 1993, John Wiley & Sons, Inc.
8. Minkiewicz, G., Russler, P., "Dynamic Response of Low Aspect Ratio Blades in a Two Stage Transonic Compressor" AIAA 97-3284