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	Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles 期刊论文 OAI收割 Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103 作者: Luo CT(罗长童); Hu ZM(胡宗民); Zhang SL; Jiang ZL(姜宗林) 收藏 \| 浏览/下载：40/0 \| 提交时间：2016/01/07 Aerodynamic coefficient Data correlation Scaling parameter Genetic programming Invariant
	Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300 会议论文 OAI收割 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012 作者: Qi DW; He GW(何国威); Liu YM 收藏 \| 浏览/下载：61/0 \| 提交时间：2013/02/26 Aerospace engineering Deformation Exhibitions Flexible wings Reynolds number Rigidity Vortex flow Aerodynamic forces Chord-based Reynolds number Flexural rigidities Free stream Free-stream flow Lattice boltzmann Leading-edge vortices Lift coefficient Lift force Particle methods Pitch rate Power efficiency Reduced frequency Three dimensional space Time-periods Tip edge Trailing edges Trailing vortex
	Analysis of microwave backscatter measured by radar altimeter on land to study surface aerodynamic roughness 会议论文 OAI收割 Land Surface Remote Sensing, Bellingham Yang, Le; Liu, Qinhuo 收藏 \| 浏览/下载：20/0 \| 提交时间：2014/12/07 Land Altimetry aerodynamic surface roughness backscatter coefficient GENERAL-CIRCULATION MODELS ZERO-PLANE DISPLACEMENT LENGTH HEIGHT EMISSION SIB
	A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文 OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏 \| 浏览/下载：74/0 \| 提交时间：2013/03/25 In this paper a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime but not accurate enough in the supersonic regime. 2011 IEEE.
	Improvement of an Aerodynamic Roughness Model With Meteorological Measurements and TM Image 会议论文 OAI收割 Zhou Y. L.; Sun X. M.; Ju W. M. 收藏 \| 浏览/下载：27/0 \| 提交时间：2012/06/30 aerodynamic roughness footprint TM image drag coefficient energy fluxes
	A wind-tunnel study of windbreak drag 期刊论文 OAI收割 AGRICULTURAL AND FOREST METEOROLOGY, 2003, 卷号: 118, 期号: 1-2, 页码: 75-84 作者: Guan, DX; Zhang, YS; Zhu, TY; Guan, DX, Chinese Acad Sci, Inst Appl Ecol, Shenyang 110016, Peoples R China \| 收藏 \| 浏览/下载：25/0 \| 提交时间：2011/09/23 Realistic Windbreak Two-dimensional Windbreak Optical Porosity Aerodynamic Porosity Drag Coefficient
	A wind-tunnel study of windbreak drag 期刊论文 OAI收割 AGRICULTURAL AND FOREST METEOROLOGY, 2003, 卷号: 118, 期号: 1-2, 页码: 75-84 Guan, DX; Zhang, YS; Zhu, TY 收藏 \| 浏览/下载：43/0 \| 提交时间：2011/09/23 realistic windbreak two-dimensional windbreak optical porosity aerodynamic porosity drag coefficient