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Concept of non-ablative thermal protection system for hypersonic vehicles 期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
作者:  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(5046Kb)  |  收藏  |  浏览/下载：1380/493  |  提交时间：2013/04/07
Flow Fields  Flow Visualization  Hypersonic Aerodynamics  Hypersonic Vehicles  Mach Number  Shock Waves  Thermal Insulating Materials  Engineering Applications  Experimental Datum  Hypersonic Wind Tunnels  Numerical Results  Stagnation Points  Thermal Protection  Thermal Protection System  Working Pressures  
The Basis of an Industry-standard Aerodynamic Computation and its Theoretical Basis with Inferences and Applications 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
作者:  Gao Z(高智)
浏览  |  Adobe PDF(780Kb)  |  收藏  |  浏览/下载：536/150  |  提交时间：2014/03/11
Numerical Simulation  Hypersonic Flow  Viscous-inviscid Interacting Shear Flow (Isf)  Cfd Validation  Wall Momentum-energy Criteria