×
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
工程热物理研究所 [11]
清华大学 [4]
北京航空航天大学 [4]
北京大学 [3]
大连化学物理研究所 [2]
力学研究所 [1]
更多...
内容类型
期刊论文 [18]
会议论文 [9]
发表日期
2018 [2]
2017 [3]
2016 [4]
2015 [2]
2013 [4]
2012 [2]
更多...
学科主题
Aircraft E... [1]
Turbomachi... [1]
Turbomachi... [1]
力学 [1]
×
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27条,第1-10条
帮助
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
作者升序
作者降序
题名升序
题名降序
发表日期升序
发表日期降序
提交时间升序
提交时间降序
Numerical investigation of effect of vortex generators on Bump inlet performance [涡流发生器对Bump进气道性能影响数值研究]
期刊论文
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 2476-2482
作者:
He, T.
;
Wang, Q.
收藏
  |  
浏览/下载:7/0
  |  
提交时间:2019/12/30
Ducts
Flow control
Flow separation
Intake systems
Vortex flow
Bump inlet
External flow fields
Numerical investigations
Off-design points
Total pressure distortion
Total pressure recovery coefficient
Total-pressure loss
Vortex generators
Computational fluid dynamics
Numerical study on boundary layer suction at throat of a CARET inlet [一种CARET进气道喉部附面层抽吸数值研究]
期刊论文
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 2278-2284
作者:
He, T.
;
Wang, Q.
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Computational fluid dynamics
Flow control
Flow fields
Flow separation
Recovery
Boundary layer interaction
Boundary layer suction
CARET inlet
Inlet performance
Throat section
Total pressure distortion
Total pressure recovery
Total pressure recovery coefficient
Boundary layers
A high-order model of rotating stall in axial compressors with inlet distortion
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017
Lin, Peng
;
Wang, Cong
;
Wang, Yong
收藏
  |  
浏览/下载:9/0
  |  
提交时间:2017/12/03
Axial compressors
Dynamic modeling
Flow instability
Inlet distortion
Rotating stall
Stall inception
CIRCUMFERENTIAL FLOW DISTORTION
STABILITY
FAN/COMPRESSORS
INSTABILITY
INCEPTION
An Improved Perceptual MBSS Noise Reduction with an SNR-Based VAD for a Fully Operational Digital Hearing Aid
期刊论文
IEICE TRANSACTIONS ON INFORMATION AND SYSTEMS, 2017
Guo, Zhaoyang
;
Wang, Xin&apos
;
Wang, Bo
;
Yong, Shanshan
;
an
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2017/12/03
digital hearing aid
noise reduction
multiband spectral subtraction
voice activity detection
SPECTRAL SUBTRACTION METHOD
SPEECH ENHANCEMENT
COLORED NOISE
Design optimization of a three-dimensional diffusing S-duct using a modified SST turbulent model
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 63-72
作者:
Gan, Wenbiao
;
Zhang, Xiaocui
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2019/12/30
S-duct
Design optimization
Modified SST turbulent model
Separation
Flow distortion
Total pressure recovery
90°方形弯管内部流动稳定性研究
期刊论文
2016, 2016
窦华书
;
牛琳
;
曹树良
;
DOU Hua-Shu
;
NIU Lin
;
CAO Shu-Liang
收藏
  |  
浏览/下载:4/0
Study of Cycle Output Improvement by Work-Fluid Including Phase Change Material
期刊论文
2016
作者:
Morita, S., Tanimura, K., Hayamizu, Y., Yamada, T., Horibe, A., Haruki, N. and Setoguchi, T.
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2017/05/27
Phase change material Heat transfer Output improvement Low temperature difference engine Thermodynamics Engineering
Numerical Investigation of Effect of Inlet Swirl and Total-pressure Distortion on Performance and Stability of an Axial Transonic Compressor
期刊论文
2016
作者:
Naseri, A., Boroomand, M. and Sammak, S.
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2017/05/27
Axial Compressors Total-Pressure Distortion Inlet Swirl Combined Distortion Performance Stability stall inception flow rotor mechanism fan Thermodynamics
Effects of Total Pressure Inlet Distortion on Transonic Fan Blade Wake Properties
会议论文
作者:
Anthony M. Ferrar, William Schneck III, Alfred Wicks, and Walter O’Brien
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2017/08/16
Analysis of Turbofan Performance Under Total Pressure Distortion at Various Operating Points
会议论文
ASME, 2015
作者:
David B. Weston
;
Matthew L. Marshall
;
Steven E. Gorrell
;
Carol V. Wallis
收藏
  |  
浏览/下载:19/0
  |  
提交时间:2016/01/25
©版权所有 ©2017 CSpace - Powered by
CSpace