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北京航空航天大学 [26]
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会议论文 [13]
期刊论文 [13]
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2019 [2]
2018 [3]
2017 [1]
2016 [3]
2015 [2]
2014 [2]
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专题:北京航空航天大学
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Discussion on correlation between wind tunnel test and flight of Mars reentry vehicle [火星再入飞行器风洞试验与真实飞行之间相关性的探讨]
期刊论文
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2019, 卷号: 45, 页码: 787-795
作者:
Liu, F.
;
Yuan, J.
收藏
  |  
浏览/下载:7/0
  |  
提交时间:2019/12/30
Aerodynamics
Correlation methods
Enthalpy
Extrapolation
Heat transfer
Hypersonic aerodynamics
Hypersonic vehicles
Numerical methods
Reentry
Testing
Wind stress
Aerodynamic forces
Aerothermodynamics
Correlation parameters
Extrapolation methods
Flight environment
Mars
Performance parameters
Pressure coefficients
Wind tunnels
Shape optimization and experimental research of near space airship
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 233, 页码: 3589-3602
作者:
Ma, Dongli
;
Li, Guanxiong
;
Yang, Muqing
;
Wang, Shaoqi
;
Zhang, Liang
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Near-space airship
low Reynolds number
aerodynamic optimization
genetic algorithm
wind tunnel test
Wind tunnel test and gust load alleviation of flexible wing including geometric nonlinearities with servo control
会议论文
AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 2018-01-08
作者:
Chao, A.
;
Changchuan, X.
;
Yang, M.
;
Chao, Y.
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Aspect ratio
Atmospheric turbulence
Aviation
Control nonlinearities
Control surfaces
Finite element method
Flexible wings
Linearization
Proportional control systems
State space methods
Structural dynamics
Two term control systems
Wind stress
Geometric non-linearity
Gust load alleviation
Nonlinear finite element method
Proportional integral derivative controllers
State - space models
Trailing-edge control surfaces
Vertical accelerations
Vortex lattice method
Wind tunnels
Assessment of Grids and Computational Schemes for Numerical Simulation of HIFiRE-5
会议论文
Proceedings of 2018 9th International Conference on Mechanical and Aerospace Engineering, ICMAE 2018
作者:
Han, Z.
;
Yan, C.
;
Liu, H.
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2019/12/30
Aerospace engineering
Boundary layer flow
Boundary layers
Discrete event simulation
Hypersonic flow
Numerical methods
Numerical models
Wind tunnels
Calculation results
Complex flow structures
Computational schemes
Grid resolution
HIFiRE-5
Reconstruction method
Spatial discretization methods
Wind tunnel test models
Computational fluid dynamics
Effect of Pitch Angle and Reynolds Number on Aerodynamic Characteristics of a Small Horizontal Axis Wind Rotor
期刊论文
JOURNAL OF APPLIED FLUID MECHANICS, 2018, 卷号: 11, 页码: 613-620
作者:
Zhu, J. Y.
;
Liu, P. Q.
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Wind energy
Horizontal axis wind rotor
Reynolds number
Aerodynamic characteristics
Wind tunnel test
Gust load alleviation wind tunnel tests of a large-aspect-ratio flexible wing with piezoelectric control
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 页码: 292-309
作者:
Bi Ying
;
Xie Changchuan
;
An Chao
;
Yang Chao
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Active control
Aeroelastic wing
Gust load alleviation
Gust response
Piezoelectric actuators
Wind tunnel test
Investigation on dynamic characteristic of a mini angle of attack sensor for small UAV
会议论文
AIAA Atmospheric Flight Mechanics Conference, 2016-01-04
作者:
Wu, D.
;
Tan, Z.
;
Zhong, Y.
;
Yang, S.
;
Song, L.
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Angle of attack
Angle of attack indicators
Antennas
Boundary layers
Computational fluid dynamics
Flight dynamics
Frequency domain analysis
Time domain analysis
Unmanned aerial vehicles (UAV)
Wind stress
Aerodynamic characteristics
Angle-of-attack sensor
Boundary layer effects
Dynamic characteristics
Small unmanned aerial vehicles
Test data analysis
Theoretical methods
Wind tunnel tests
Wind tunnels
Gust response analysis and wind tunnel test for a high-aspect ratio wing
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 页码: 91-103
作者:
Liu Yi
;
Xie Changchuan
;
Yang Chao
;
Cheng Jialin
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Gust loads
High-aspect ratio wing
Nonlinear analysis
Unsteady vortex lattice method (UVLM)
Wind tunnels
Geometrically Nonlinear Aeroelastic Stability Analysis and Wind Tunnel Test Validation of a Very Flexible Wing
期刊论文
SHOCK AND VIBRATION, 2016, 卷号: 2016
作者:
Xie, Changchuan
;
Liu, Yi
;
Yang, Chao
;
Cooper, J. E.
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2019/12/30
Design and analysis of a wind tunnel test model system for rolling maneuver load alleviation of flying wings
会议论文
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015, Kissimmee, FL, United states, 2015-01-05
作者:
Yin, Huiwei
;
Wu, Zhigang
;
Yang, Chao
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2020/01/06
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