机译:优化内部冷却通道压力损失的U型弯头-第一部分:数值方法
von Karman Institute for Fluid Dynamics, Turbomachinery and Propulsion Department, Chaussee de Waterloo 72, Rhode-Saint-Genese 1640, Belgium;
von Karman Institute for Fluid Dynamics, Turbomachinery and Propulsion Department, Chaussee de Waterloo 72, Rhode-Saint-Genese 1640, Belgium,Mechanical Engineering Department, Stanford University, Stanford, CA;
von Karman Institute for Fluid Dynamics, Turbomachinery and Propulsion Department, Chaussee de Waterloo 72, Rhode-Saint-Genese 1640, Belgium,Tractable Engineering, Brussels, Belgium;
von Karman Institute for Fluid Dynamics, Turbomachinery and Propulsion Department, Chaussee de Waterloo 72, Rhode-Saint-Genese 1640, Belgium,Geosea NV, Zwijndrecht, Belgium;
von Karman Institute for Fluid Dynamics, Turbomachinery and Propulsion Department, Chaussee de Waterloo 72, Rhode-Saint-Genese 1640, Belgium;
机译:在内部冷却通道中使压力损失最小的U型弯头的优化-第二部分:实验验证
机译:发动机相似横截面的带肋双通道内部冷却通道180°弯曲时压力损失和传热的数值研究
机译:发动机相似横截面的带肋双通道内部冷却通道180°弯曲时压力损失和传热的数值研究
机译:内部冷却通道中最小压力损失的U型弯的优化-第一部分:数值方法
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:顺序冷冻剂喷射冷却和激光照射的数值优化改善葡萄酒污染治疗
机译:静止旋转状态矩阵冷却几何传热和压力损失估计的数值框架