Forced response prediction methodology for the design of HP compressors bladed disks

Proceedings of the ASME Turbo Expo 2004

Volumn 6, Issue , 2004, Pages 317-326

  Seinturier, Eric ^a   Lombard, Jean Pierre ^a   Dumas, Michel ^a   Dupont, Christian ^a   Sharma, Virendra ^a   Dupeux, Jérôme ^a  

^a SNECMA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CRACKS; DISKS (MACHINE COMPONENTS); PARAMETER ESTIMATION; TURBINES; TURBOMACHINE BLADES;

AEROELASTIC DAMPING; COMPRESSOR BLADED DISKS; FLIGHT DOMAIN; HIGH CYCLE FATIGUE;

COMPRESSORS;

EID: 10244246657     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-53372     Document Type: Conference Paper

References (13)

1. R. Bladh, M.P Castanier and C. Pierre (2001) "Component mode based reduced order modeling techniques for mistuned bladed disks - Part I & II", Journal of Engineering for Gas Turbine and Power, Vol. 123, pp 89-108.
2. M. Berthillier, C. Dupont, P.Chanez, F. Saurat (1998) "Réponse forcée aéroélastique des aubes de turbomachines", Revue Française de Mécanique, Vol. 1998/04.
3. M. P. Castanier, G. Ottarsson, C. Pierre (1997) "A reduced order Modeling Technique for Mistuned Bladed Disks", ASME Journal of Vibration and Acoustics, Vol. 119 (3), pp. 439-447.
4. J.C. Chassaing, G.A. Gerolymos: "Compressor Flutter Analysis using time nonlinear and time linearized 3D Navier-Stokes Methods", ISUAAAT, Lyon (France), 2000
5. E.F. Crawley : "Aeroelastic formulation for Tuned and Mistuned Rotors" AGARD Manual on Aeroelasticity in Axial Flow Turbomachines, Vol. 2, Structural Dynamics and Aeroelasticity
6. G.A. Gerolymos, G. Tsanga, I. Vallet: "Near Wall k-ε Computational of Transonic Turbomachinery Flows With Tip Clearance" AIAA Journal, Vol. 36, 1998, pp 1769-1777
7. G.A. Gerolymos "Advanced in the Numerical Integration of the 3D Euler Equations for Vibrating Cascades", ASME paper 92GT170.
8. th Biennial Conference on Mechanical Vibrations and Noise, September 2003, Chicago
9. W. Ning, S. Moffatt, Y. Li, R.G. Wells, "Blade Forced Response Prediction For Industrial Gas Turbines - Part 2: verification and application", ASME/IGTI TurboExpo GT2003-38642, Atlanta, 2003.
10. th International Conference On Damage Assessment Of Structures (DAMAS), Cardiff, 2001.
11. A.I. Sayma, M. Vahdati, S.J. Lee, M. Imregun, "Overview Of Shaft Driven Lift Fan Forced Response Analyses", HCF Conference, Miami, 2002.
12. E. Seinturier, C. Dupont, M. Berthillier, M. Dumas (2000) "A new method to predict flutter in presence of structural mistuning", ISUAAAT 2000, Lyon, France
13. E. Seinturier, J.P. Lombard, M. Berthillier, O. Sgarzi (2002) "Turbine Mistuned Forced Response Prediction - Comparison With Experimental Results", ASME-IGTI Turboexpo GT-2002-30424, Amsterdam, The Netherlands