机译:低温推进剂甲烷超临界湍流对流换热的数值研究
Zhejiang University, 310027 Hangzhou, People's Republic of China School of Aeronautics and Astronautics;
rnZhejiang University, 310027 Hangzhou, People's Republic of China School of Aeronautics and Astronautics;
rnZhejiang University, 310027 Hangzhou, People's Republic of China School of Aeronautics and Astronautics;
A: surface area, m~2; A_n: coefficients in the Benedict-Webb-Rubin equation; C_p: constant-pressure heat capacity, J kg~(-1) K~(-1); C_v: constant-volume heat capacity, J kg~(-1) K~(-1); D: diameter of the tube, m; et al;
机译:低温推进剂甲烷超临界湍流对流换热的数值研究
机译:矩形发动机冷却通道中低温推进剂甲烷的超临界传热
机译:不同超临界压力下强制对流中的空间发育湍流传热的数值研究
机译:基于整体法的超临界流体流动湍流对流传热的数值研究
机译:百叶窗对带有过渡湍流的凹窗对流传热速率影响的数值研究
机译:恒定热通量等边三角形管道中利用纳米流体的层流和对流换热的数值研究
机译:水平管中超临界压力流体湍流对流传热的数值模型
机译:湍流对流换热过渡到超临界氦气流