中国科学院机构知识库网格系统: 检索

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	Deducing Aerodynamic Roughness Length From Abundant Anemometer Tower Data to Inform Wind Resource Modeling 期刊论文 OAI收割 GEOPHYSICAL RESEARCH LETTERS, 2024, 卷号: 51, 期号: 21, 页码: 11 作者: Wang, Jiamin; Yang, Kun; Yuan, Ling; Liu, Jiarui; Peng, Zhong \| 收藏 \| 浏览/下载：6/0 \| 提交时间：2025/03/03 aerodynamic roughness length wind resource modeling anemometer towers
	Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文 OAI收割 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21 作者: Yang L(杨磊); Ye, Zhengyin; Li WH(李文皓); Sun QH(孙泉华) \| 收藏 \| 浏览/下载：40/0 \| 提交时间：2021/11/01 Store separation Aerodynamic modeling Interference aerodynamics Dynamic simulation Air-launch-to-orbit
	Force measurement in a shock tunnel with 100 milliseconds test duration 会议论文 OAI收割 34th AIAA Applied Aerodynamics Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016 作者: Wang YP(汪运鹏); Liu YF(刘云峰); Luo ZT(罗长童); Jiang ZL(姜宗林) 收藏 \| 浏览/下载：39/0 \| 提交时间：2017/05/05 Aerodynamic forces Chinese Academy of Sciences Different structure Digital filtering Large scale modeling Low frequency vibration Strain gauge balances Strain gauge sensors
	Sensitivity analysis of Aerodynamic Roughness Length on Surface Air Temperature in Eastern China 会议论文 OAI收割 Proceedings of the 2013 the International Conference on Remote Sensing, Environment and Transportation Engineering (Rsete 2013) Zuo, Jingying; Qi, Yuanyuan; Lu, Lixin 收藏 \| 浏览/下载：27/0 \| 提交时间：2014/12/07 Aerodynamic roughness length RAMS Regional climate modeling CLIMATE MODEL
	Establishment of airplane flight model and simulation analysis of landing behavior (EI CONFERENCE) 会议论文 OAI收割 2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China 作者: Li L.; Li M. 收藏 \| 浏览/下载：25/0 \| 提交时间：2013/03/25 This paper create a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation for accurately analyzing the performance and influence of landing gear system. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic aerodynamic landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing and it is actual in the physical process. 2011 IEEE.
	Aircraft landing gear simulation using multidomain modeling technology (EI CONFERENCE) 会议论文 OAI收割 2011 International Conference on Information Technology, Computer Engineering and Management Sciences, ICM 2011, September 24, 2011 - September 25, 2011, Nanjing, Jiangsu, China 作者: Li M. 收藏 \| 浏览/下载：40/0 \| 提交时间：2013/03/25 In order to accurately analyze the performance and influence of landing gear system this paper presents a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic aerodynamic landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing and it is improve the precision of flight simulation. 2011 IEEE.