机译:摩擦减阻通风局部腔边界层分析
Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China;
Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China;
Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China;
Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China|Zhejiang Univ State Key Lab Fluid Power & Mech Syst Hangzhou 310027 Peoples R China;
Zhejiang Univ Ocean Coll Zhoushan 316021 Peoples R China;
Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China|Shanghai Ship & Shipping Res Inst Shanghai 200135 Peoples R China;
Drag reduction; Boundary layers; Gas-liquid multiphase flow; Ventilated partial cavity; Large eddy simulation;
机译:腔内制度的实验性和数值研究和通风局部腔的减阻
机译:基于双流体模型的通风局部空腔减阻的数值研究
机译:通风局部腔下游的微泡减阻
机译:通过空气层和部分腔减少皮肤摩擦减少
机译:层流和湍流边界层中的皮肤摩擦阻力减小。
机译:外围膜蛋白在支持的脂质双层上的横向扩散受1)结合脂质和2)渗透到双层烃核中的蛋白质结构域的累加摩擦阻力控制
机译:超声边界层氢气注射液的皮肤摩擦减阻研究
机译:通过使用边界层加热减少飞机巡航阻力以最小化机身皮肤摩擦