机译:薄膜孔轴排布局叶片层压端壁冷却特性的实验研究
Univ Sci &
Technol China CAS Key Lab Mech Behav &
Design Mat Dept Thermal Sci &
Energy Engn 96 Jinzhai Rd Hefei 230027 Anhui Peoples R China;
Univ Sci &
Technol China CAS Key Lab Mech Behav &
Design Mat Dept Thermal Sci &
Energy Engn 96 Jinzhai Rd Hefei 230027 Anhui Peoples R China;
Univ Sci &
Technol China CAS Key Lab Mech Behav &
Design Mat Dept Thermal Sci &
Energy Engn 96 Jinzhai Rd Hefei 230027 Anhui Peoples R China;
Aviat Ind Corp China Aeroengine Inst 1 Wanlian Rd Shenyang 110015 Liaoning Peoples R China;
Aviat Ind Corp China Aeroengine Inst 1 Wanlian Rd Shenyang 110015 Liaoning Peoples R China;
Turbine vane end-wall; Laminated cooling; Temperature ratio; Over cooling effectiveness; Thermal gradient;
机译:薄膜孔轴排布局叶片层压端壁冷却特性的实验研究
机译:自由流湍流强度效应对各种内部销翅片配置的叶片层压末端壁的整体冷却性能和固体热变形的实验研究
机译:交错抗倾斜薄膜孔和铺设背形孔扭叶片薄膜冷却和传热特性的实验研究
机译:涡轮叶片全覆盖膜冷却特性的实验研究
机译:槽膜冷却燃气轮机喷嘴导向叶片内壁空气动力学和传热的实验性和数值研究
机译:燃气轮机叶片前缘旋流膜冷却的共轭传热研究
机译:壁厚和孔形变形效应对燃气轮机叶片全覆盖薄膜冷却性能的实验研究
机译:层合多孔板材流动,氧化,冷却和热疲劳特性的实验研究