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	Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions 会议论文 OAI收割 Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019 作者: Prapamonthon P; Yin B(银波); Yang GW(杨国伟); Zhang MH(张莫晗); Yang GW(杨国伟) \| 收藏 \| 浏览/下载：41/0 \| 提交时间：2020/11/20 Aerothermal condition Cooling effectiveness Cooling performance Thermal sensitivity Turbine vane
	Aerodynamic and Aerothermal Performance of Power-law Shaped Leading Edge of Hypersonic Waveriders 期刊论文 OAI收割 Procedia Engineering, 2013, 卷号: 67, 页码: 207-217 作者: Wang FM(王发民); Han HQ(韩汉桥); Lei MF(雷麦芳); Zhang J(张杰) 收藏 \| 浏览/下载：30/0 \| 提交时间：2015/09/24 aerothermal protection power-law leading edge aerodynamic performance
	Aerodynamic and Aerothermal Performance of Power-law Shaped Leading Edge of Hypersonic Waveriders 会议论文 OAI收割 7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013 作者: Wang FM(王发民); Han HQ(韩汉桥); Lei MF(雷麦芳); Zhang J(张杰); Wang FM(王发民) 收藏 \| 浏览/下载：22/0 \| 提交时间：2014/03/11 hypersonic aerothermal protection power-law leading edge aerodynamic performance
	Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm 会议论文 OAI收割 23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19 作者: Cui K(崔凯); Hu SC(胡守超); Gao TY(高太元); Wang XP(王秀平); Yang GW(杨国伟) 收藏 \| 浏览/下载：14/0 \| 提交时间：2014/04/02 vehicle leading 0algorithm genetic hypersonic optimization aerothermal based method design attack novel around angle evaluated greatly about fluid result differ
	Thermal-structure analysis of supersonic dome based on three materials (EI CONFERENCE) 会议论文 OAI收割 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China Jiang Z.; Ai X.; Wei Q.; Liu B.; Jia H. 收藏 \| 浏览/下载：25/0 \| 提交时间：2013/03/25 To a supersonic missile a seeker could enhance the aerodynamic ability due to decrease the resistance in flying. At the same time the primary function of a seeker has been considered as the most important equipment for a missile due to the importance for cueing of targets and tracking for the final approach. However the dome of a seeker which is made up of glass has poor mechanical performance. Especially in the higher altitude for a dome in which the aerothermal and pressure loads could destroy the structure easily it is necessary to do the thermal-structure coupled analysis due to varied materials. In the paper to take the spherical dome of a seeker as a example the analysis has been completed according to the varied materials consist of MgF2 Al2O3 and ZnS. The temperature loads and the pressure loads derived from the results of fluent analysis has been forced on the surface of dome which simulates the actual Mach 2.5 in flying. According to the results of coupled analysis the SEQV stress of the dome radium 80mm based on three materials had reached to 31MPa which shows that the strength is sufficient for Mach 2.5 and offered the warranty to design the attaching to missile for the dome. At the same time the results required the flexible mounting for the dome due to the displacements results which the crystal material couldn't accept. 2011 IEEE.
	AITEB - An European Research Project on Aero-thermodynamics of Turbine Endwalls and Blades 期刊论文 OAI收割 JOURNAL OF THERMAL SCIENCE, 2004, 卷号: 13, 期号: 2, 页码: 97,108 F. HASELBACH; H.-P. SCHIFFER 收藏 \| 浏览/下载：17/0 \| 提交时间：2013/03/11 turbines aerothermal endwalls blades cooling-technology experiment CFD.
	AITEB - An European Research Project on Aero-thermodynamics of Turbine Endwalls and Blades 期刊论文 OAI收割 JOURNAL OF THERMAL SCIENCE, 2004, 卷号: 13, 期号: 2, 页码: 97,108 作者: F. HASELBACH; H.-P. SCHIFFER \| 收藏 \| 浏览/下载：9/0 \| 提交时间：2013/03/11 Turbines Aerothermal Endwalls Blades Cooling-technology Experiment Cfd.