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Volumn 31, Issue 5, 2010, Pages 761-764

Boundary layer transition prediction and mechanism analysis of a high-loading LP turbine blade profile

Author keywords

Boundary layer transition; Free stream turbulence level; Long separation bubble; Numerical investigation

Indexed keywords

BLADE SUCTION; BOUNDARY LAYER TRANSITIONS; BOUNDARY-LAYER SEPARATION; FREESTREAM TURBULENCE; LP TURBINES; MECHANISM ANALYSIS; NUMERICAL INVESTIGATIONS; NUMERICAL MODELS; NUMERICAL RESULTS; PROFILE LOSS; RE NUMBERS; SEPARATION BUBBLE; STATIC PRESSURE; TRANSITION MODEL;

EID: 77953155156     PISSN: 0253231X     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (3)

References (6)
  • 1
    • 10244225954 scopus 로고    scopus 로고
    • Aerodynamics of a low-pressure turbine airfoil under steady and periodically unsteady conditions
    • Canada: Carleton University
    • Mahallati A. Aerodynamics of a low-pressure turbine airfoil under steady and periodically unsteady conditions [D]. Canada: Carleton University, 2003
    • (2003)
    • Mahallati, A.1
  • 2
    • 0028486598 scopus 로고
    • Two-equation eddy-viscosity turbulence models for engineering applications
    • Menter F R. Two-equation eddy-viscosity turbulence models for engineering applications [J]. AIAA-Journal, 1994, 32: 1598-1605
    • (1994) AIAA-Journal , vol.32 , pp. 1598-1605
    • Menter, F.R.1
  • 3
    • 33845684578 scopus 로고    scopus 로고
    • A correlation-based transition model using local variables-Part 1: Model formulation
    • Menter F R, Langtry F B, Likki S R, et al. A correlation-based transition model using local variables-Part 1: Model formulation [J]. ASME J. Turbomachinery, 2006, 128: 413-422
    • (2006) ASME J. Turbomachinery , vol.128 , pp. 413-422
    • Menter, F.R.1    Langtry, F.B.2    Likki, S.R.3
  • 4
    • 77953150047 scopus 로고    scopus 로고
    • A correlation-based transition model using local variables-Part 2: test cases and industrial applications
    • Menter F R, Langtry F B, Likki S R, et al. A correlation-based transition model using local variables-Part 2: test cases and industrial applications [J]. ASME J. Turbomachinery, 2006, 129: 14-22
    • (2006) ASME J. Turbomachinery , vol.129 , pp. 14-22
    • Menter, F.R.1    Langtry, F.B.2    Likki, S.R.3
  • 6
    • 33750881176 scopus 로고    scopus 로고
    • Aerodynamics of a family of three highly loaded low-pressure turbine airfoils: Measured effects of Reynolds number and turbulence intensity in steady flow
    • GT2006-91271
    • Popovic, Zhu J W, Dai, Sjolander S A. Aerodynamics of a family of three highly loaded low-pressure turbine airfoils: Measured effects of Reynolds number and turbulence intensity in steady flow [CP/DK]. ASME Turbo Expo 2006: Power for Land, Sea and Air, 2006, GT2006-91271
    • (2006) ASME Turbo Expo 2006: Power for Land, Sea and Air
    • Popovic1    Zhu, J.W.2    Dai3    Sjolander, S.A.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.