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机译:燃气轮机叶片前缘复合角膜冷却的数值模拟
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an, China;
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an, China;
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an, China;
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an, China;
School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an, China;
Compound angle; Film cooling; Leading edge; Numerical simulations; Turbine blade;
机译:燃气轮机叶片前缘模型冲击和薄膜复合冷却的数值模拟
机译:涡轮叶片前缘冷却通道模型中喷嘴长径比和喷嘴角度对涡流冷却影响的数值研究
机译:薄雾法对涡轮叶片前缘高效薄膜冷却的数值模拟
机译:吹气比对燃气轮机前缘膜冷却结构的膜冷却效率和传热系数的影响的实验和数值研究
机译:管表面LIGA热交换器的制造和分析:涡轮叶片前缘区域的冷却模拟。
机译:燃气轮机叶片前缘旋流膜冷却的共轭传热研究
机译:吹气比对燃气轮机叶片前缘薄膜冷却结构中薄膜冷却效率和传热系数影响的实验和数值研究
机译:涡轮喷气发动机空气冷却涡轮叶片的实验研究Ⅵ - 转子叶片牵引和牵引边缘的导热和薄膜冷却