机译:氢的湍流边界层燃烧的表皮摩擦和传热预测理论的改进
Beihang Univ, Sch Aeronaut Sci & Engn, Natl Lab Computat Fluid Dynam, Beijing, Peoples R China;
Beihang Univ, Sch Aeronaut Sci & Engn, Natl Lab Computat Fluid Dynam, Beijing, Peoples R China;
Univ Michigan, Sch Aeronaut & Astronaut, Ann Arbor, MI 48109 USA;
Beihang Univ, Sch Aeronaut Sci & Engn, Natl Lab Computat Fluid Dynam, Beijing, Peoples R China;
Beihang Univ, Sch Aeronaut Sci & Engn, Natl Lab Computat Fluid Dynam, Beijing, Peoples R China;
Boundary-layer combustion; Skin friction; Heat transfer; Theoretical analysis; Numerical simulation;
机译:“改善氢气的湍流边界层燃烧的皮肤摩擦和传热预测理论”的更正[Int J Hydrogen Energy 42(2017)26123-26131]
机译:氢的边界层燃烧控制高超声速湍流皮肤摩擦
机译:高超音速湍流边界层燃料的喷射和燃烧:减少皮肤摩擦的机理
机译:铆钉对高速湍流边界层中皮肤摩擦和传热的影响
机译:具有恒定壁温加热和增加热通量边界条件的光滑管中具有可变特性的空气和氩气湍流的局部和平均传热特性的试验摩擦系数和平均摩擦系数。
机译:量热燃烧和甲苯燃烧热的改进
机译:通过氢的边界层燃烧控制高超声速湍流皮肤摩擦
机译:高压湍流在Ogive-Cylinder上的摩擦力和传热预测。