Analytical solutions of velocity and temperature in laminar boundary layer over a flat plate with wall injection flow using HPM-Padé method

被引：0
|
作者：
Zhao, Guo-Chang [1 ,3 ]
Kong, Jing-Ru [1 ]
Song, Li-Ping [2 ]
Du, Xia [1 ]
Shan, Long [1 ]
Zhao, Heng [1 ]
机构：
[1] Faculty of Aerospace Engineering, Shenyang Aerospace University, Shenyang,110136, China
[2] Science and Technology Association, Shenyang Aerospace University, Shenyang,110136, China
[3] Liaoning Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System, Faculty of Aerospace Engineering, Shenyang Aerospace University, Shenyang,110136, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2015年 / 30卷 / 08期
关键词：
D O I：
10.13224/j.cnki.jasp.2015.08.001
中图分类号：
学科分类号：
摘要：
14
引用
收藏
页码：1793 / 1801
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