연구동향 분석

터빈 동익 흡입면에서 발달하는 경계층의 유동특성

장성일(Sung Il Chang) 이상우(Sang Woo Lee) 2015년

논문상세정보
인용/피인용
' 터빈 동익 흡입면에서 발달하는 경계층의 유동특성' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 기계공학
  • boundarylayer(경계층)
  • energyspectrum(에너지스펙트럼)
  • separated-flow transition(박리유동 천이)
  • suction surface(흡입면)
  • turbine blade(터빈 동익)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
932 0

0.0%

' 터빈 동익 흡입면에서 발달하는 경계층의 유동특성' 의 참고문헌

  • Turbulent Boundary Layer Growth over a Longitudinally Curved Surface
    Meroney, R. N. AIAA J. 13 : 1448 ~ 1453 [1975]
  • Turbulence
    Hinze, J. O. McGraw-Hill [1956]
  • Turbine Separation Control Using Pulsed Vortex, Generator Jets
    Bons, J. P. ASME J. of Turbomachinery 123 : 198 ~ 206 [2001]
  • Transition Mechanisms in laminar Separated Flow Under Simulated low Pressure Turbine Airfoil Conditions
    Dahnert, J. ASME J. of Turbomachinery 135 : 011007-1 ~ 011007-10 [2013]
  • Tip Gap Flow Characteristics in a Turbine Cascade Equipped with Pressure-Side Partial Squealer Rims
    Lee, S. W. Int. J. of Heat and Fluid Flow 50 : 369 ~ 377 [2014]
  • The Velocity Field of the Turbulent Very Near Wake of a Circular Cylinder
    Ong, L. Experiments in Fluids 20 : 441 ~ 453 [1996]
  • The Role of Laminar-Turbulent Transition in Gas Turbine Engines
    Mayle, R. E. ASME J. of Turbomachinery 113 : 509 ~ 537 [1991]
  • Subminiature Hot-Wire Sensors: Development and Use
    Ligrani, P. M. J. of Physics. E 20 : 323 ~ 332 [1987]
  • Separated Flow Transition Under Simulated low-Pressure Turbine Airfoil Conditions-Part 2: Turbulence Spectra
    Volino, R. J. ASME J. of Turbomachinery 124 : 656 ~ 664 [2002]
  • Separated Flow Transition Under Simulated low-Pressure Turbine Airfoil Conditions-Part 1: Mean Flow and Turbulence Statistics
    Volino, R. J. ASME J. of Turbomachinery 124 : 645 ~ 655 [2002]
  • Measurements of Endwall Heat (Mass) Transfer Coefficient ina Linear Turbine Cascade Using Naphthalene Sublimation Technique
    Jun, S. B. Kumoh National Institute of Technology [2000]
  • Measurements in Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions
    Volino, R. J. ASME J. of Turbomachinery 123 : 189 ~ 197 [2001]
  • Effects of Surface Roughness and Turbulence Intensity on the Aerodynamic Losses Produced by the Suction Surface of a Simulated Turbine Airfoil
    Zhang, Q. ASME J. of Fluids Engineering 126 : 257 ~ 265 [2004]
  • Effects of Incidence Angle on Endwall Convective Transport Within a High-Turning Turbine Rotor Passage
    Lee, S. W. Int. J. of Heat and Mass Transfer 52 : 5922 ~ 5931 [2009]
  • Effects of Combustor-Level High Free-Stream Turbulence on Blade-Surface Heat/Mass Transfer in the Three-Dimensional Flow Region near the Endwall of a High-Turning Turbine Rotor Blade
    Lee, S. W. J. of Mech. Sci. and Tech. 19 : 1347 ~ 1357 [2005]
  • Effect of Surface Roughness and Free-stream Turbulence on the Wake Turbulence Structure of a Symmetric Airfoil
    Zhang, Q. Physics of Fluids 16 (6) : 2044 ~ 2053 [2004]
  • Aerodynamics of a Low-Pressure Turbine Airfoil at Low Reynolds numbers-Part II: Blade-Wake Interaction
    Mahallati, A. ASME J. of Turbomachinery 135 : 011011-1 ~ 011011-10 [2013]
  • Aerodynamics of a Low-Pressure Turbine Airfoil at Low Reynolds numbers-Part I:Steady Flow Measurements
    Mahallati, A. ASME J. of Turbomachinery 135 : 011010-1 ~ 011010-9 [2013]