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A Comparative Study of Heat Transfer between Rotating Circular Smooth-Walled and Square Rib-Roughened Ducts with Cooling Application for Gas Turbine Rotor Blades.

机译：燃气涡轮转子叶片旋转圆形光滑壁围墙和方形肋粗糙粗糙粗糙型管道的比较研究。

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Shyy Woei CHANG; W.David MORRIS;
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年度 1998
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1. Effects of Rib Arrangements on Heat Transfer and Flow Behavior in a Rectangular Rib-Roughened passage: Application to Cooling of Gas Turbine Blade Trailing Edge [J] . Robert Kiml, Sadanari Mochizuki, Akira Murata Journal of Heat Transfer . 2001,第4期

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2. Large Eddy Simulation of Flow and Heat Transfer in the Developing Flow Region of a Rotating Gas Turbine Blade Internal Cooling Duct With Coriolis and Buoyancy Forces [J] . Evan A. Sewall, Danesh K. Tafti Journal of turbomachinery . 2008,第1期

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3. Impingement cooling in a rotating curved square annular duct with crossflow effect from Rib-roughened surfaces [J] . Shou-Shing Hsieh, Jung-Tai Huang, Huang-Hsiu Tsai Heat and mass transfer . 2003,第2期

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4. HEAT TRANSFER IN A RIB-ROUGHENED ROTATING TWIN-PASS TRAPEZOIDAL-SECTIONED PASSAGE WITH COOLING APPLICATION TO GAS TURBINE ROTOR BLADE [C] . Shyy Woei Chang, Tsun Lirng Yang, Yu Ker-Wei, International Conference on Fast Sea Transportation . 2006

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5. Experimental Heat Transfer Coefficients and Friction Factors in a Rib-Roughened Leading-Edge Cooling Cavity of a Gas Turbine Airfoil. [D] . Hagan, Peter. 2013

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7. Influence of the Gap Size Between Side Walls and Ribs on the Heat Transfer in a Stationary and Rotating Straight Rib-roughened Duct [O] . R. Kiml, S. Mochizuki, A. Murata 2000

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8. Influence of Cooling Air Injection on Flow Development and Heat Transfer in a Rotating Leading Edge Coolant Duct of a Film-Cooled Turbine Blade [R] . Elfert, M. 2003

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A Comparative Study of Heat Transfer between Rotating Circular Smooth-Walled and Square Rib-Roughened Ducts with Cooling Application for Gas Turbine Rotor Blades.

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