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Volumn 6, Issue , 2004, Pages 563-572

Linear stability analysis of LPT rotor packets - Part ii: Three-dimensional results and mistuning effects

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CANTILEVER BEAMS; DAMPING; LINEAR SYSTEMS; TURBINES;

EID: 10244250403     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-54120     Document Type: Conference Paper
Times cited : (8)

References (15)
  • 1
    • 0000104175 scopus 로고
    • Thin layer approximation and algebraic model for separated flows
    • Huntsville, Alabama
    • Baldwin, B.S., and Lomax, H. "Thin Layer Approximation and algebraic model for Separated Flows", AIAA 16th Aerospace Science Meeting, Huntsville, Alabama, 1978.
    • (1978) AIAA 16th Aerospace Science Meeting
    • Baldwin, B.S.1    Lomax, H.2
  • 3
    • 84894562431 scopus 로고    scopus 로고
    • Validation of a linear multigrid accelerated unstructured navier-stokes solver for the computation of turbine blades on hybrid grids
    • Corral, R., Escribano, A., Gisbert, F., Serrano, A., and Vasco, C., "Validation of a Linear Multigrid Accelerated Unstructured Navier-Stokes Solver for the Computation of Turbine Blades on Hybrid Grids" AIAA Paper 2003-3326, 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.3326
    • Corral, R.1    Escribano, A.2    Gisbert, F.3    Serrano, A.4    Vasco, C.5
  • 4
    • 10244253951 scopus 로고    scopus 로고
    • Linear stability analysis of LPT rotor packets - Part I: Methodology and two-dimensional results
    • Corral, R., Lopez, C, and Vasco, C. "Linear Stability Analysis of LPT Rotor Packets - Part I: Methodology and Two-dimensional Results", ASME Paper 2004-GT-54119, 2004.
    • (2004) ASME Paper 2004-GT-54119
    • Corral, R.1    Lopez, C.2    Vasco, C.3
  • 5
    • 0002102788 scopus 로고
    • Aeroelastic formulation of tuned and mistuned rotor
    • Structural Dynamics and Aeroelasticity
    • Crawley, E.F., "Aeroelastic Formulation of Tuned and Mistuned Rotor", AGARD Manual on Aeroelasticity in Axial Flow Turbomachines", Vol. 2, Structural Dynamics and Aeroelasticity, pp. 19-1, 19-24, 1987.
    • (1987) AGARD Manual on Aeroelasticity in Axial Flow Turbomachines , vol.2 , pp. 19-21
    • Crawley, E.F.1
  • 6
    • 0348226379 scopus 로고    scopus 로고
    • Mistuning identification of bladed discs using a fundamental mistuning model - Part i: Theory
    • Feiner, D.M., and Griffin, J.H., "Mistuning Identification of Bladed discs Using A Fundamental Mistuning Model - Part I: Theory", ASME Paper GT-2003-38952, 2003.
    • (2003) ASME Paper GT-2003-38952
    • Feiner, D.M.1    Griffin, J.H.2
  • 7
    • 0019916969 scopus 로고
    • Flutter and response of a mistuned cascade in incompressible flow
    • Kaza, K.R.V.,and Kielb,R.E., "Flutter and Response of a Mistuned Cascade in Incompressible Flow", AIAA Journal, Vol. 20, No. 8, pp. 1120-1127, 1982.
    • (1982) AIAA Journal , vol.20 , Issue.8 , pp. 1120-1127
    • Kaza, K.R.V.1    Kielb, R.E.2
  • 8
    • 84905734755 scopus 로고    scopus 로고
    • Experimental study of the aerodynamic and structural damping in a full-scale rotating turbine
    • Kielb, J.J., and Abhari, R.S., "Experimental Study of the Aerodynamic and Structural Damping in a Full-Scale Rotating Turbine", ASME Paper 2001-GT-0262, 2001.
    • (2001) ASME Paper 2001-GT-0262
    • Kielb, J.J.1    Abhari, R.S.2
  • 12
    • 0034818920 scopus 로고    scopus 로고
    • Computation of mistuning effects on cascade flutter
    • January
    • Sadeghi, M., and Liu, F., "Computation of Mistuning Effects on Cascade Flutter", AIAA Journal, Vol. 39, No. 1, pp. 22-28, January 2001
    • (2001) AIAA Journal , vol.39 , Issue.1 , pp. 22-28
    • Sadeghi, M.1    Liu, F.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.