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Heat Transfer With Film Cooling Within and Downstream of One to Four Rows of Normal Injection Holes

机译：在一到四排正常注射孔的内部和下游的薄膜冷却和下游的传热

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D. E. Metzger; P. A. Kuenstler; D. I. Takeuchi;
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年度 1976
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2. LES of rotational effects on film cooling effectiveness and heat transfer coefficient in a gas turbine blade with one row of air film injection [J] . Al-Zurfi Nabeel, Turan Ali International Journal of Thermal Sciences . 2016,第Null期

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3. Investigation of film cooling effectiveness and heat transfer coefficient for rectangular holes with two rows [J] . Ibrahim Koç Yasar Islamoglu Ünal Akdag Aircraft Engineering and Aerospace Technology . 2009,第2期

机译：两排矩形孔的薄膜冷却效率和传热系数的研究
4. INTERACTION OF FILM COOLING ROWS: EFFECTS OF HOLE GEOMETRY AND ROW SPACING ON THE COOLING PERFORMANCE DOWNSTREAM OF THE SECOND ROW OF HOLES [C] . Christian Saumweber, Achmed Schulz Heat Transfer . 2003

机译：膜冷却行的相互作用：孔的几何形状和行距对第二个孔的冷却性能下降的影响
5. An experimental and numerical investigation of heat transfer downstream of a normal film cooling injection slot. [D] . Sun, Yuping. 1995

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6. Conjugate Heat Transfer Investigation on Swirl-Film Cooling at the Leading Edge of a Gas Turbine Vane [O] . Haifen Du, Ziyue Mei, Jiayao Zou, 2019

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7. Heat transfer, adiabatic effectiveness and injectant distributions downstream of single rows and two staggered rows of film-cooling holes with simple and compound angles [O] . Jackson Stephen Mark 1991

机译：单排和两排交错的薄膜冷却孔的传热，绝热效果和喷射剂分布的下游，角度简单且复合

Heat Transfer With Film Cooling Within and Downstream of One to Four Rows of Normal Injection Holes

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