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机译:大肋距间距肋板式通道内流动与传热的实验与数值研究
Engineering Simulation and Aerospace Computing (ESAC), Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Northwestern Polytechnical University, Xi'an, 710072, Shaanxi, China,Division of Heat Transfer, Department of Energy Sciences, Lund University, P.O. Box 118, SE-22100, Lund, Sweden;
Division of Heat Transfer, Department of Energy Sciences, Lund University, P.O. Box 118, SE-22100, Lund, Sweden;
Engineering Simulation and Aerospace Computing (ESAC), Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Northwestern Polytechnical University, Xi'an, 710072, Shaanxi, China;
Division of Heat Transfer, Department of Energy Sciences, Lund University, P.O. Box 118, SE-22100, Lund, Sweden;
cooling channel; heat transfer enhancement; rib turbulator; large pitch-to-height ratio; liquid crystal thermography (LCT); numerical simulation;
机译:长宽比,通道方向,肋距高度比和肋壁数量对带肋的旋转通道中压降特性的影响
机译:长宽比,通道方向,肋距高度比和肋壁数量对带肋的旋转通道中压降特性的影响
机译:肋角和肋骨取向对双通罗纹通道流动和热传递的影响
机译:薄膜孔相对位置对带罗丝横流冷却液通道薄膜冷却膜冷却效果的实验和数值研究
机译:涡轮机翼型冷却通道传热的组合数值和实验研究,具有成角度肋和180度U型弯曲转动
机译:乙醇/聚α-烯烃纳米乳液流经圆形微通道的流动和传热特性的实验研究
机译:纵横比,沟道取向,肋间距到高比率的影响,肋壁的旋转沟槽中的压降特性数量