Results 221 to 230 of about 60,335 (265)
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Film-Cooling Performance and Heat Transfer over an Inclined Film-Cooled Surface
Journal of Thermophysics and Heat Transfer, 2008Experiments 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 flow. The vertical temperature distribution was measured to infer the flow structure and the rate of mixing of the film jet with the ...
C. S. Yang, C. L. Lin, C. Gau
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Film Cooling Effectiveness for Short Film Cooling Holes Fed by a Narrow Plenum
Journal of Turbomachinery, 1999The adiabatic, steady-state liquid crystal technique was used to measure surface adiabatic film cooling effectiveness values in the near-hole region X/D<10. A parametric study was conducted for a single row of short holes L/D⩽3 fed by a narrow plenum H/D=1.
C. A. Hale +2 more
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Double-Jet Ejection of Cooling Air for Improved Film Cooling
Journal of Turbomachinery, 2006Film cooling in gas turbines leads to aerodynamic mixing losses and reduced temperatures of the gas flow. Improvements of the gas turbine thermal efficiency can be achieved by reducing the cooling fluid amount and by establishing a more equal distribution of the cooling fluid along the surface.
Karsten Kusterer +3 more
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1954
Thin liquid wall films flowing under the influence of high-velocity turbulent gas streams were studied for the purpose of obtaining an understanding of the mechanics of film cooling. Conditions which insure liquid-film attachment to solid surfaces without loss of unevaporated liquid to the gas stream when simple radial-hole injectors are used were ...
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Thin liquid wall films flowing under the influence of high-velocity turbulent gas streams were studied for the purpose of obtaining an understanding of the mechanics of film cooling. Conditions which insure liquid-film attachment to solid surfaces without loss of unevaporated liquid to the gas stream when simple radial-hole injectors are used were ...
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The Cooling Index: An Integral Measure of Film Cooling Performance
Heat Transfer in Gas Turbines, 1994Abstract A simple measure of film cooling performance is presented to aid the preliminary design of gas turbines. The Cooling Index, CI, is defined as the reduction in total heat load due to the film cooling divided by the baseline (no film cooling) heat load over a specified area of a turbine blade, ΔQ˙fc/Q˙bl.
Robert P. Campbell, Robert J. Moffat
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2000
Es handelt sich um eine spezielle Methode zur Kuhlung von Oberflachen (engl.: heat protection), bei der durch diskrete Oberflachenoffnungen ein Fluidfilm zwischen das heise Gas der Ausenstromung und die Wand eingeblasen wird. Es besteht physikalisch eine enge Verwandtschaft zur sog. TranspirationskUhlung.
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Es handelt sich um eine spezielle Methode zur Kuhlung von Oberflachen (engl.: heat protection), bei der durch diskrete Oberflachenoffnungen ein Fluidfilm zwischen das heise Gas der Ausenstromung und die Wand eingeblasen wird. Es besteht physikalisch eine enge Verwandtschaft zur sog. TranspirationskUhlung.
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Adiabatic Film Cooling Effectiveness Measurements Throughout Multi-Row Film Cooling Arrays
Volume 5C: Heat Transfer, 2016Adiabatic film cooling effectiveness measurements are obtained using pressure-sensitive paint (PSP) on a flat film cooled surface. The effects of blowing ratio and hole spacing are investigated for four multi-row arrays comprised of 8 rows containing 52 holes of 3.8 mm diameter with 20° inclination angles and hole length-to-diameter ratio of 11.2.
Greg Natsui +5 more
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Cooling of coupled solids by helium films
Physical Review Letters, 1992Recently, Mester et al. have made measurements of the cooling effect of a superfluid He film on a composite bolometer. In interpreting their results they suggest that the main thermal resistance is caused by an insufficient generation of excitations, which can cause evaporation, in the He film. In this Letter we suggest an alternative explanation which
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Effect of Rotation on Flow Field and Film Cooling Effectiveness in Film-Cooled Turbine Rotors
International Journal of Turbo & Jet-Engines, 2014AbstractExperimental and numerical investigations of flow field in a film-cooled turbine model under stationary and rotating conditions in a low-speed wind tunnel are conducted. The effects of different blowing ratios (M = 1.5, 2) on the flow field are studied.
Xiaocheng Zhu, Liangliang Liu, Feng Yuan
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Numerical Analysis of Film-Cooling Performance and Optimization for a Novel Shaped Film-Cooling Hole
Volume 4: Heat Transfer, Parts A and B, 2012In the present work, a numerical study on a novel shaped film-cooling hole has been performed. The novel shaped hole is designed to enhance lateral spreading of coolant on the cooling surface. The film-cooling performance of the novel shaped hole is compared with the fan, laidback fan, and dumbbell shaped film-cooling holes at density ratio of 1.75 in ...
Ki-Don Lee, Sun-Min Kim, Kwang-Yong Kim
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