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Volumn 20, Issue 3, 2005, Pages 355-360

Simulation of boundary layer transition

Author keywords

Aerospace propulsion system; Boundary layer transition; Flat plate; Simulation; Turbine

Indexed keywords

AEROSPACE VEHICLES; CASCADES (FLUID MECHANICS); COMPUTER SIMULATION; PLATES (STRUCTURAL COMPONENTS); PROPULSION; TURBINES; TURBULENT FLOW;

EID: 22844440441     PISSN: 10008055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (15)

References (11)
  • 1
    • 2942727482 scopus 로고    scopus 로고
    • Reduction of separation losses on a turbine blade with low Reynolds number
    • AIAA 99-0242
    • Lake J P, King P I, Rivir R B. Reduction of Separation Losses on a Turbine Blade With Low Reynolds Number[R]. AIAA 99-0242.
    • Lake, J.P.1    King, P.I.2    Rivir, R.B.3
  • 2
    • 0030408820 scopus 로고    scopus 로고
    • Turbulence modeling with application to turbomachinery
    • Bradshaw P. Turbulence Modeling with Application to Turbomachinery[J]. Progress in Aerospace Science, 1996, 32(6): 575-624.
    • (1996) Progress in Aerospace Science , vol.32 , Issue.6 , pp. 575-624
    • Bradshaw, P.1
  • 3
    • 0003741690 scopus 로고
    • Transition, pressure gradient and stability theory
    • Report ES 26388, Douglas Aircraft Co., EI Segundo, California
    • Smith AMO, Gamberoni N. Transition, Pressure Gradient and Stability Theory[R]. Report ES 26388, Douglas Aircraft Co., EI Segundo, California, 1956.
    • (1956)
    • Smith, A.M.O.1    Gamberoni, N.2
  • 4
    • 0019070772 scopus 로고
    • Natural transition of boundary layers - The effect of turbulence, pressure gradient, and flow history
    • Abu-Ghannam B J, Shaw R. Natural Transition of Boundary Layers-The Effect of Turbulence, Pressure Gradient, and Flow History[J]. Journal of Mechanical Engineering and Science, 1980, 22(5): 213-228.
    • (1980) Journal of Mechanical Engineering and Science , vol.22 , Issue.5 , pp. 213-228
    • Abu-Ghannam, B.J.1    Shaw, R.2
  • 5
    • 84924787284 scopus 로고
    • The role of laminar-turbulent transition in gas turbine engines
    • Mayle R E. The Role of Laminar-Turbulent Transition in Gas Turbine Engines[J]. ASME Journal of Turbomachinery, 1991, 113: 509-537.
    • (1991) ASME Journal of Turbomachinery , vol.113 , pp. 509-537
    • Mayle, R.E.1
  • 6
    • 22844440767 scopus 로고    scopus 로고
    • Experimental research on transition phenomenon of a compressor cascade and a new empirical criterion for transition modeling
    • JIANG Hongde, ZHONG Yongxing, LING Junyang. Experimental Research on Transition Phenomenon of a Compressor Cascade and a New Empirical Criterion for Transition Modeling[J]. Journal of Engineering Thermophysics, 1996, 17(4): 433-436.
    • (1996) Journal of Engineering Thermophysics , vol.17 , Issue.4 , pp. 433-436
    • Jiang, H.1    Zhong, Y.2    Ling, J.3
  • 7
    • 22844442152 scopus 로고    scopus 로고
    • Numerical investigation into transitional flow
    • Beijing: Chinese Academy of Sciences Institute of Engineering Thermophysics
    • XU Xingzhong. Numerical Investigation into Transitional Flow[D]. Beijing: Chinese Academy of Sciences Institute of Engineering Thermophysics, 1996.
    • (1996)
    • Xu, X.1
  • 8
    • 22844433006 scopus 로고    scopus 로고
    • Study of numerical simulation method of transition to viscous flow in turbomachinery
    • Harbin: Harbin Institute of Technology
    • GUO Yubo. Study of Numerical Simulation Method of Transition to Viscous Flow in Turbomachinery[D]. Harbin: Harbin Institute of Technology, 2001.
    • (2001)
    • Guo, Y.1
  • 9
    • 0141707344 scopus 로고    scopus 로고
    • Application of GMRES algorithm in the predictions of two-dimensional turbulent steady flow
    • NING Fangfei, XU Liping. Application of GMRES Algorithm in the Predictions of Two-Dimensional Turbulent Steady Flow[J]. ACTA Mechanics SINICA, 2001, 33(4): 442-451.
    • (2001) ACTA Mechanics SINICA , vol.33 , Issue.4 , pp. 442-451
    • Ning, F.1    Xu, L.2
  • 10
    • 0141818629 scopus 로고    scopus 로고
    • Numerical investigation of transonic compressor rotor flow using an implicit 3D flow solver with one-equation Spalart-Allmaras turbulence model
    • ASME 2001-GT-0359
    • Ning F, Xu L. Numerical Investigation of Transonic Compressor Rotor Flow Using an Implicit 3D Flow Solver with One-Equation Spalart-Allmaras Turbulence Model[R]. ASME 2001-GT-0359.
    • Ning, F.1    Xu, L.2
  • 11
    • 22844436150 scopus 로고    scopus 로고
    • Detailed velocity and turbulence measurements of profile boundary layer in a large scale turbine cascade
    • ASME No. 96-GT-42
    • Ubaldi M, Zunino P, Campora U, Ghiglione A. Detailed Velocity and Turbulence Measurements of Profile Boundary Layer in a Large Scale Turbine Cascade[R]. ASME No. 96-GT-42.
    • Ubaldi, M.1    Zunino, P.2    Campora, U.3    Ghiglione, A.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.