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Volumn 6 PART A, Issue , 2006, Pages 553-562

Numerical simulation of the flow interaction between turbine main annulus and disc cavities

Author keywords

[No Author keywords available]

Indexed keywords

BLADING AERODYNAMICS; DISC CAVITIES; STAGNATION TEMPERATURE;

EID: 33750880624     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2006-90307     Document Type: Conference Paper
Times cited : (38)

References (20)
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    • (1989) ASME Journal of Turbomachinery , vol.113 , pp. 91-97
    • Chew, J.W.1
  • 4
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    • Rim seal experiments and analysis of a rotor-stator system with non-axisymmetric main flow
    • no. 92-GT-160
    • Hamabe, K., and Ishida, K., 1992. "Rim seal experiments and analysis of a rotor-stator system with non-axisymmetric main flow". In Proceedings of the ASME Turbo Expo, no. 92-GT-160.
    • (1992) Proceedings of the ASME Turbo Expo
    • Hamabe, K.1    Ishida, K.2
  • 7
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    • A simple method for estimating ingestion of annulus gas into a turbine rotor-stator cavity in the presence of external pressure variations
    • no. GT2004-53097
    • Scanlon, T., Wilkes, J., Bohn, D., and Gentilhomme, O., 2004. "A simple method for estimating ingestion of annulus gas into a turbine rotor-stator cavity in the presence of external pressure variations". In Proceedings of the ASME Turbo Expo, no. GT2004-53097.
    • (2004) Proceedings of the ASME Turbo Expo
    • Scanlon, T.1    Wilkes, J.2    Bohn, D.3    Gentilhomme, O.4
  • 8
    • 84928498865 scopus 로고    scopus 로고
    • Influence of rim seal geometry on hot gas ingestion into the upstream cavity of an axial turbine stage
    • no. 99-GT-248
    • Bohn, D., Rudzinski, B., Surken, N., and Gartner, W., 1999. "Influence of rim seal geometry on hot gas ingestion into the upstream cavity of an axial turbine stage". In Proceedings of the ASME Turbo Expo, no. 99-GT-248.
    • (1999) Proceedings of the ASME Turbo Expo
    • Bohn, D.1    Rudzinski, B.2    Surken, N.3    Gartner, W.4
  • 10
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    • Pressure field and main stream gas ingestion in a rotor-stator disc cavity
    • no. 2001-GT-564
    • Roy, R. P., Xu, G., Feng, J., and Kang, S., 2001. "Pressure field and main stream gas ingestion in a rotor-stator disc cavity". In Proceedings of the ASME Turbo Expo, no. 2001-GT-564.
    • (2001) Proceedings of the ASME Turbo Expo
    • Roy, R.P.1    Xu, G.2    Feng, J.3    Kang, S.4
  • 14
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    • The importance of shroud leakage modelling in multistage turbine flow calculations
    • no. GT2005-68459
    • Rosic, B., Denton, J. D., and Pullan, G., 2005. "The importance of shroud leakage modelling in multistage turbine flow calculations". In Proceedings of the ASME Turbo Expo, no. GT2005-68459.
    • (2005) Proceedings of the ASME Turbo Expo
    • Rosic, B.1    Denton, J.D.2    Pullan, G.3
  • 15
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    • Analytical investigation of a low pressure turbine with and without flowpath endwall gaps, seals and clearance features
    • no. GT2005-68492
    • Cherry, D., Wadia, A., Beacock, R., Subramanian, M., and Vitt, P., 2005. "Analytical investigation of a low pressure turbine with and without flowpath endwall gaps, seals and clearance features". In Proceedings of the ASME Turbo Expo, no. GT2005-68492.
    • (2005) Proceedings of the ASME Turbo Expo
    • Cherry, D.1    Wadia, A.2    Beacock, R.3    Subramanian, M.4    Vitt, P.5
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    • A one-equation turbulence model for aerodynamic flows
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    • (1994) La Recherche Aerospatiale , vol.1 , pp. 5-21
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.