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您的检索式：作者名="SHAO Yetao"
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| 1 | Continuous Detonation Engine and Effects of Different Types of Nozzle on Its Propulsion Performance显示文摘The rotating propagation of a continuous detonation engine(CDE) with different types of nozzles is investigated in three-dimensional numerical simulation using a one-step chemical reaction model.Flux terms are solved by the so-called monotonicity-preserving weighted essentially non-oscillatory(MPWENO) scheme.The simulated flow field agrees well with the previous experimental results.Once the initial transient effects die down,the detonation wave maintains continuous oscillatory propagation in the annular chamber as long as fuel is continuously injected.Using a numerical flow field,the propulsion performance of a CDE is computed for four types of nozzles,namely the constant-area nozzle,Laval nozzle,diverging nozzle and converging nozzle.The gross specific impulse of the CDE ranges 1 540-1 750 s and the mass flux per square meter ranges 313-330 kg/(m2·s) for different nozzles.Among these four types of nozzles,Laval nozzle performs the best,and these parameters are 1 800 N,1 750 s and 313 kg/(m2·s).A nozzle can greatly improve the propulsion performance. | Shao Yetao Liu Meng Wang Jianping | 2010 | Chinese Journal of Aeronautics2010，23，6： | 26 |
| 2 | The Reliable and Intelligent Propulsion Pressurization System of the Long March 7 Launch Vehicle显示文摘The reliable and intelligent propulsion pressurization system is one of the key technologies of new Chinese generation launch vehicles; a high reliability design is an important guarantee for the success of launching. This paper analyzes the domestic and overseas liquid launch vehicles in the area of propulsion pressurization systems, based on comprehensive analysis, demonstrating the reliable and intelligent propulsion pressurization system of the Long March 7(Simplified as LM-7) has been raised. By applying a full chain redundancy design, setting proper pressure control bandwidth and control mode reconstruction under extreme fault conditions, the reliability and adaptability of the propulsion pressurization system has enhanced significantly. In addition, the complete system has been verified by the first two flights of LM-7. | FAN Ruixiang DENG Xinyu SHAO Yetao YANG Haoliang TIAN Yurong | 2017 | Aerospace China2017，18，4： | 1 |
| 3 | Induction of Pluripotency in Mouse Somatic Cells with Lineage Specifiers显示文摘 | Jian Shu Chen Wu Yetao Wu Zhiyuan Li Sida Shao Wenhui Zhao Xing Tang Huan Yang Lijun Shen Xiaohan Zuo Weifeng Yang Yan Shi Xiaochun Chi Hongquan Zhang Ge Gao Youmin Shu Kehu Yuan Weiwu He Chao Tang Yang Zhao Hongkui Deng | 2013 | Cell2013，，5： | 1 |
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