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Volumn 10, Issue , 2006, Pages 7535-7542

Role of tip clearance flow in the generation of non-synchronous vibrations

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; PRESSURE GRADIENT; ROTORS; TURBOMACHINE BLADES; VIBRATION CONTROL; VIBRATIONS (MECHANICAL);

EID: 34250730734     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-629     Document Type: Conference Paper
Times cited : (34)

References (12)
  • 1
    • 0343231932 scopus 로고
    • Non-Engine Order Blade Vibration in a High Pressure Compressor
    • ISABE Paper 95-7094
    • Baumgartner, M., Kamaler, F. and Hourmouziadis, J., "Non-Engine Order Blade Vibration in a High Pressure Compressor," ISABE Paper 95-7094, 1995.
    • (1995)
    • Baumgartner, M.1    Kamaler, F.2    Hourmouziadis, J.3
  • 2
    • 0346965589 scopus 로고    scopus 로고
    • Blade Excitation by Aerodynamic Instabilites - A Compressor Blade Study
    • Kielb, R.E., Thomas, J.P., Barter, J.W. and Hall, K.C., "Blade Excitation by Aerodynamic Instabilites - A Compressor Blade Study," ASME Paper GT-2003-38634, 2003.
    • (2003) ASME Paper , vol.GT-2003-38634
    • Kielb, R.E.1    Thomas, J.P.2    Barter, J.W.3    Hall, K.C.4
  • 5
    • 0013382322 scopus 로고    scopus 로고
    • Role of Tip Clearance Flow on Axial Compressor Stability
    • Ph.D. Dissertation, Massachusetts Institute of Technology, Cambridge, MA
    • Vo, H. D., "Role of Tip Clearance Flow on Axial Compressor Stability", Ph.D. Dissertation, Massachusetts Institute of Technology, Cambridge, MA, 2001.
    • (2001)
    • Vo, H.D.1
  • 6
    • 27744436794 scopus 로고    scopus 로고
    • Vo, .H. D., Tan, C.S. and Greitzer, E.M., 2005, Criteria for Spike Initiated Rotating Stall, ASME paper GT2005-68374, presented at ASME IGTI Turbo Expo 2005, Reno-Tahoe, Nevada, June 2005. (Accepted for publication in the ASME Journal of Turbomachinery)
    • Vo, .H. D., Tan, C.S. and Greitzer, E.M., 2005, "Criteria for Spike Initiated Rotating Stall," ASME paper GT2005-68374, presented at ASME IGTI Turbo Expo 2005, Reno-Tahoe, Nevada, June 2005. (Accepted for publication in the ASME Journal of Turbomachinery)
  • 8
    • 0343960744 scopus 로고
    • NASA LEWIS Research Center, Data and Performance Report for the Best Stage Configuration, NASA CR-165357
    • Wisler, D.C., "Core Compressor Exit Stage Study," NASA LEWIS Research Center, Volume IV- Data and Performance Report for the Best Stage Configuration, NASA CR-165357, 1981.
    • (1981) Core Compressor Exit Stage Study , vol.4
    • Wisler, D.C.1
  • 10
    • 0042635994 scopus 로고
    • Discussion of Benser W. A.: Transonic Compressor Technology Advancements
    • Part II, NASA SP-304
    • Koch, C. C., "Discussion of Benser W. A.: Transonic Compressor Technology Advancements," Fluid Mechanics, Acoustics, and Design of Turbomachinery, Part II, NASA SP-304, 1974.
    • (1974) Fluid Mechanics, Acoustics, and Design of Turbomachinery
    • Koch, C.C.1
  • 12
    • 0019548731 scopus 로고
    • Dynamics of an Impinging Jet. Part 1. The Feedback Phenomenon
    • Ho, C.-M. and Nosseir, N.S., "Dynamics of an Impinging Jet. Part 1. The Feedback Phenomenon," Journal of Fluid Mechanics, Vol 105, 1981, pp.119-142.
    • (1981) Journal of Fluid Mechanics , vol.105 , pp. 119-142
    • Ho, C.-M.1    Nosseir, N.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.