메뉴 건너뛰기




Volumn 118, Issue 2, 1996, Pages 181-188

Effects of rotating inlet distortion on multistage compressor stability

Author keywords

[No Author keywords available]

Indexed keywords


EID: 4243147574     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2836624     Document Type: Article
Times cited : (89)

References (21)
  • 1
    • 0024731506 scopus 로고
    • Calculations of Inlet Distortion Induced Compressor Flowfield Instability
    • Chue, R., Hynes, T. P., Greitzer, E. M., Tan, C. S., and Longley, J. P., 1989, “Calculations of Inlet Distortion Induced Compressor Flowfield Instability,” Int. J. Heat Fluid Flow, Vol. 10, No. 3.
    • (1989) Int. J. Heat Fluid Flow , vol.10 , Issue.3
    • Chue, R.1    Hynes, T.P.2    Greitzer, E.M.3    Tan, C.S.4    Longley, J.P.5
  • 2
    • 0027187717 scopus 로고
    • Stall Inception in Axial Flow Compressors
    • Day, I. J., 1993a, “Stall Inception in Axial Flow Compressors,” ASME Journal of Turbomachinery, Vol. 115, pp. 1-9.
    • (1993) ASME Journal of Turbomachinery , vol.115 , pp. 1-9
    • Day, I.J.1
  • 3
    • 0027148134 scopus 로고
    • Active Suppression of Rotating Stall and Surge in Axial Compressors
    • Day, I. J., 1993b, “Active Suppression of Rotating Stall and Surge in Axial Compressors,” ASME Journal of Turbomachinery, Vol. 115, pp. 40-47.
    • (1993) ASME Journal of Turbomachinery , vol.115 , pp. 40-47
    • Day, I.J.1
  • 6
    • 0026143130 scopus 로고
    • Rotating Waves as a Stall Inception Indication in Axial Compressors
    • Gamier, V. H., Epstein, A. H., and Greitzer, E. M., 1991, “Rotating Waves as a Stall Inception Indication in Axial Compressors,” ASME Journal of Turbomachinery, Vol. 113, pp. 290-301.
    • (1991) ASME Journal of Turbomachinery , vol.113 , pp. 290-301
    • Gamier, V.H.1    Epstein, A.H.2    Greitzer, E.M.3
  • 7
    • 0345905941 scopus 로고
    • Dynamic Control of Rotating Stall in Axial Flow Compressors Using Aeromechanical Feedback
    • Aug
    • Gysling, D. L., 1993, “Dynamic Control of Rotating Stall in Axial Flow Compressors Using Aeromechanical Feedback,” MIT Gas Turbine Laboratory Report No. 219, Aug.
    • (1993) MIT Gas Turbine Laboratory Report , pp. 219
    • Gysling, D.L.1
  • 8
    • 84925954798 scopus 로고
    • Active Stabilization of Rotating Stall in a Three-Stage Axial Compressor
    • Haynes, J. M., Hendricks, G. J., and Epstein, A. H., 1994, “Active Stabilization of Rotating Stall in a Three-Stage Axial Compressor,” ASME Journal of Turbomachinery, Vol. 116, pp. 226-239.
    • (1994) ASME Journal of Turbomachinery , vol.116 , pp. 226-239
    • Haynes, J.M.1    Hendricks, G.J.2    Epstein, A.H.3
  • 9
    • 0023384319 scopus 로고
    • A Method for Assessing Effects of Inlet Flow Distortion on Compressor Stability
    • Hynes, T. P., and Greitzer, E. M., 1987, “A Method for Assessing Effects of Inlet Flow Distortion on Compressor Stability,” ASME Journal of Turbomachinery, Vol. 109, pp. 371-379.
    • (1987) ASME Journal of Turbomachinery , vol.109 , pp. 371-379
    • Hynes, T.P.1    Greitzer, E.M.2
  • 10
    • 0020943365 scopus 로고
    • Aspects of the Appearance and Elimination of Breakdown in an Axial-Flow Compressor in the Presence of a Rotating Non-uniformity at the Inlet
    • (translated)
    • Kozarev, L. A., and Federov, R. M., 1983, “Aspects of the Appearance and Elimination of Breakdown in an Axial-Flow Compressor in the Presence of a Rotating Non-uniformity at the Inlet,” Izevstiya vuz Aviatsionnaya Tekhnika, Vol. 26(1), pp. 33-37 (translated).
    • (1983) Izevstiya Vuz Aviatsionnaya Tekhnika , vol.26 , Issue.1 , pp. 33-37
    • Kozarev, L.A.1    Federov, R.M.2
  • 11
    • 1542759850 scopus 로고    scopus 로고
    • Measured and Predicted Effects of Inlet Distortion on Axial Compressors
    • 90-GT-214
    • Longley, J. P., “Measured and Predicted Effects of Inlet Distortion on Axial Compressors,” ASME Paper No. 90-GT-214.
    • ASME Paper
    • Longley, J.P.1
  • 12
    • 0027962752 scopus 로고
    • A Review of Nonsteady Flow Models for Compressor Stability
    • Longley, J. P., 1994, “A Review of Nonsteady Flow Models for Compressor Stability,” ASME Journal of Turbomachinery, Vol. 116, pp. 202-215.
    • (1994) ASME Journal of Turbomachinery , vol.116 , pp. 202-215
    • Longley, J.P.1
  • 13
    • 0025226336 scopus 로고
    • Stability of Flow Through Multistage Axial Compressors
    • Longley, J. P., and Hynes, T. P., 1990, “Stability of Flow Through Multistage Axial Compressors,” ASME Journal of Turbomachinery, Vol. 112, pp. 126-132.
    • (1990) ASME Journal of Turbomachinery , vol.112 , pp. 126-132
    • Longley, J.P.1    Hynes, T.P.2
  • 16
    • 85011609955 scopus 로고
    • Dynamic Performance of Stalled Blade Rows
    • Paper #11, presented at Tokyo Joint International Gas Turbine Conference, Tokyo, Japan, Oct
    • Nagano, S., Machida, Y., and Takata, H., 1971, “Dynamic Performance of Stalled Blade Rows,” Japan Society of Mechanical Engineering, Paper #11, presented at Tokyo Joint International Gas Turbine Conference, Tokyo, Japan, Oct.
    • (1971) Japan Society of Mechanical Engineering
    • Nagano, S.1    Machida, Y.2    Takata, H.3
  • 21
    • 0022045543 scopus 로고
    • Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing
    • Wisler, D. C., 1985, “Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, pp. 354-363.
    • (1985) ASME Journal of Engineering for Gas Turbines and Power , vol.107 , pp. 354-363
    • Wisler, D.C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.