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机译:全覆盖薄膜冷却:稀疏孔阵列在不同的吹塑比和收缩比下的传热系数和膜效率
Department of Engineering Science, University of Oxford, Oxford, UK,Eminent in Propulsion, Mechanical and Aerospace Engineering, College of Engineering, Department of Mechanical and Aerospace Engineering, Propulsion Research Center, Olin B. King Technology Hall S236, University of Alabama in Huntsville, Huntsville, AL 35899;
Department of Engineering Science, University of Oxford, Oxford, UK,Hill Air Force Base, USAF, 6030 Gum Lane, Bldg. 1217, Hill AFB, UT 84056;
Solar Turbines Inc., Heat Transfer Research, 2200 Pacific Highway, P. O. Box 85376, Mail Zone C-9, San Diego, CA 92186-5376;
Solar Turbines Inc., Heat Transfer Research, 2200 Pacific Highway, P. O. Box 85376, Mail Zone C-9, San Diego, CA 92186-5376;
film cooling; full-coverage film cooling; thermal protection; turbine; gas turbine engine; heat transfer;
机译:全覆盖薄膜冷却:在不同的孔角度,收缩率和吹塑率下,致密孔阵列的膜效率和传热系数
机译:全覆盖薄膜冷却:在不同的吹塑比下,密集和稀疏孔阵列的薄膜效率和传热系数
机译:壁厚和注射方向对平板全覆盖薄膜冷却阵列:绝热膜效果和传热系数
机译:全覆盖薄膜冷却:稀疏孔阵在不同的吹入比和收缩比下的传热系数和膜效率
机译:自由流湍流强度对反涡流孔膜冷却效率和传热系数影响的实验研究。
机译:降膜蒸发模型的建立及总传热系数的相关性
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:高自由流湍流下圆柱形薄膜孔的90度偏斜前缘薄膜冷却效率,传热和放电系数