×
验证码:
换一张
忘记密码?
记住我
CORC
首页
科研机构
检索
知识图谱
申请加入
托管服务
登录
注册
在结果中检索
科研机构
北京航空航天大学 [11]
内容类型
期刊论文 [9]
会议论文 [2]
发表日期
2018 [3]
2017 [1]
2015 [2]
2014 [3]
2013 [1]
2011 [1]
更多...
×
知识图谱
CORC
开始提交
已提交作品
待认领作品
已认领作品
未提交全文
收藏管理
QQ客服
官方微博
反馈留言
浏览/检索结果:
共11条,第1-10条
帮助
限定条件
专题:北京航空航天大学
第一署名单位
第一作者单位
通讯作者单位
已选(
0
)
清除
条数/页:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
排序方式:
请选择
发表日期升序
发表日期降序
提交时间升序
提交时间降序
题名升序
题名降序
作者升序
作者降序
Numerical study on non-locally reacting behavior of nacelle liners incorporating drainage slots
期刊论文
JOURNAL OF SOUND AND VIBRATION, 2018, 卷号: 424, 页码: 15-31
作者:
Chen, Chao
;
Li, Xiaodong
;
Thiele, Frank
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Acoustic liner
Drainage slot
High sound pressure level
Computational aeroacoustics
Numerical study on acoustic impedance variation along uniformly distributed multi-slit resonators
会议论文
AIAA Aerospace Sciences Meeting, 2018, 2018-01-08
作者:
Li, X.D.
;
Chen, C.
;
Hu, F.Q.
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2019/12/30
Acoustic field measurement
Acoustic fields
Acoustic resonators
Acoustic wave propagation
Acoustic wave reflection
Acoustic wave transmission
Aviation
Computational aeroacoustics
Ducts
Fire alarm systems
Orifices
Perforated plates
Underwater acoustics
Acoustic energy distributions
Helmholtz resonators
Impedance distribution
Impedance variations
Resistance variations
Sound pressure level
Specific frequencies
Straight-forward method
Acoustic impedance
Numerical Simulation of Supersonic Twin-Jet Noise with High-Order Finite Difference Scheme
期刊论文
22nd AIAA/CEAS Aeroacoustics Conference, 2018, 卷号: 56, 页码: 290-300
作者:
Gao, Junhui
;
Xu, Xin
;
Li, Xiaodong
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Aeroacoustics
Computational aeroacoustics
Eigenvalues and eigenfunctions
Finite difference method
Geometry
Harmonic analysis
Navier Stokes equations
Nozzles
Supersonic aerodynamics
Convective velocity
Coupling mechanism
Dynamic mode decompositions
Filtered Navier-Stokes equations
Flux reconstruction
High order finite difference schemes
High-order finite differences
Nozzle configuration
Fighter aircraft
Implementation of Delayed Detached Eddy Simulation method to a high order spectral difference solver
期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 154, 页码: 90-101
作者:
Gao, Junhui
;
Li, Xiaodong
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
High order spectral difference method
Delayed Detached Eddy Simulation
Spalart Allmaras model
Multi-time step method
Computational aeroacoustics
A Numerical Investigation on Sound Absorption Mechanism of Micro Resonator with Offset Slits
期刊论文
JOURNAL OF COMPUTATIONAL ACOUSTICS, 2015, 卷号: 23
作者:
Xu, Jun
;
Li, Xiaodong
;
Guo, Yueping
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/01/06
Computational aeroacoustics
micro resonator
offset slit
direct numerical simulation
high sound pressure level
Recent advances of computational aeroacoustics
期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2015, 卷号: 36, 页码: 131-140
作者:
Li, Xiao-dong
;
Jiang, Min
;
Gao, Jun-hui
;
Lin, Da-kai
;
Liu, Li
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
aeroacoustics
computational aeroacoustics (CAA)
high order finite difference scheme
non-reflecting boundary condition
Nonuniform-time-step explicit Runge-Kutta scheme for high-order finite difference method
期刊论文
COMPUTERS & FLUIDS, 2014, 卷号: 105, 页码: 166-178
作者:
Liu, Li
;
Li, Xiaodong
;
Hu, Fang Q.
收藏
  |  
浏览/下载:1/0
  |  
提交时间:2020/01/06
Explicit Runge-Kutta method
High order finite difference method
Computational aeroacoustics
A Study of Three-Dimensional Acoustic Scattering by Arbitrary Distribution Multibodies Using Extended Immersed Boundary Method
期刊论文
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 2014, 卷号: 136
作者:
Jiang, Yongsong
;
Wang, Xiaoyu
;
Jing, Xiaodong
;
Sun, Xiaofeng
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/01/06
computational aeroacoustics
immersed boundary method
acoustic scattering
A new computational model for circumferentially non-uniform liner
会议论文
20th AIAA/CEAS Aeroacoustics Conference 2014, Atlanta, GA, United states, 2014-06-16
作者:
Wang, Xiaoyu
;
Huang, Lixi
;
Sun, Xiaofeng
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/01/06
A block interface flux reconstruction method for numerical simulation with high order finite difference scheme
期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2013, 卷号: 241, 页码: 1-17
作者:
Gao, Junhui
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/01/06
High order finite difference method
Interface flux reconstruction
Overlap grid
Stability
Computational aeroacoustics
©版权所有 ©2017 CSpace - Powered by
CSpace