Film-cooling performance and heat transfer over an inclined film-cooled surface

被引:8
|
作者
Yang, C. S. [2 ]
Lin, C. L. [1 ]
Gau, C. [1 ]
机构
[1] Natl Cheng Kung Univ, Inst Aeronaut & Astronaut, Tainan 70101, Taiwan
[2] Far E Univ, Dept Comp Sci & Informat Engn, Tainan 74401, Taiwan
关键词
D O I
10.2514/1.32351
中图分类号
O414.1 [热力学];
学科分类号
摘要
Experiments have been performed to study and obtain the adiabatic wall film-cooling effectiveness and the heat transfer over a film-cooled surface that is made inclined at various angles with respect to a uniform How. The vertical temperature distribution was measured to infer the flow structure and the rate of mixing of the film jet with the freestream. The inclination angle of the film-cooled surface ranges from -20 to 20 deg with an increment of 5 deg, the blowing parameter from 0.5 to 2.0 (0.5,0.7, 1.0,1.5,2.0). It is found that the mixing of the film jet with the freestream is significantly affected by the inclination angle of the film-cooled surface. The divergence of the film-cooled surface can make the How unstable and cause flow separation, whereas the convergence has both stabilization and impingement effects on the film jet. This has a very complicated effect on both the film-cooling performance and the heat transfer under the film. More detailed discussion on the How and the heat transfer is presented. Correlations for both the film cooling effectiveness and the heat transfer under the film are provided.
引用
收藏
页码:485 / 492
页数:8
相关论文
共 50 条
  • [1] Film cooling performance and heat transfer over an inclined film-cooled surface at different convergent angles with respect to highly turbulent mainstream
    Yang, C. S.
    Lin, C. L.
    Gau, C.
    APPLIED THERMAL ENGINEERING, 2009, 29 (01) : 167 - 177
  • [2] Film cooling performance and heat transfer over an inclined film-cooled surface at different divergent angles with espect to the highly turbulent mainstream
    Yang, CS
    Lin, CL
    Gau, C
    PROCEEDINGS OF THE 3RD INTERNATIONAL SYMPOSIUM ON HEAT TRANSFER ENHANCEMENT AND ENERGY CONSERVATION, VOLS 1 AND 2, 2004, : 1067 - 1075
  • [3] Film cooling performance and heat transfer over an inclined film-cooled surface at different divergent angles with respect to highly turbulent mainstream
    Yang, Chih-Sheng
    Lin, C. L.
    Gau, C.
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2008, 32 (06) : 1313 - 1321
  • [4] Film-cooled turbine endwall in a transonic flow field: Part II - Heat transfer and film-cooling effectiveness
    Nicklas, M
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2001, 123 (04): : 720 - 729
  • [5] EFFECTIVENESS OF FILM-COOLING OF A FLAT WALL BY AIR INJECTION THROUGH A SLOT NORMAL TO THE FILM-COOLED SURFACE
    REPUKHOV VM
    POPOVICH YEG
    DANILEYKO VM
    1970, 2 (01): : 128 - 133
  • [6] Heat transfer on a film-cooled rotating blade
    Garg, VK
    INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2000, 21 (02) : 134 - 145
  • [7] EFFECT OF ACCELERATION ON THE HEAT-TRANSFER COEFFICIENT ON A FILM-COOLED SURFACE
    AMMARI, HD
    HAY, N
    LAMPARD, D
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1991, 113 (03): : 464 - 471
  • [8] Conjugate Heat Transfer Simulations of a Nozzle Flow over a Film-Cooled Plate
    Zore, Krishna
    Aliaga, Cristhian
    Shah, Shoaib
    Stokes, John
    Zori, Laith
    Makarov, Boris
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2023, 37 (02) : 404 - 423
  • [9] Heat Transfer Coefficient Measurements on the Film-Cooled Pressure Surface of a Transonic Airfoil
    Kodzwa, Paul M.
    Eaton, John K.
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2013, 135 (06):
  • [10] Numerical investigation of heat transfer on film-cooled turbine blades
    Ginibre, P
    Lefebvre, M
    Liamis, N
    HEAT TRANSFER IN GAS TURBINE SYSTEMS, 2001, 934 : 377 - 384