×
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 [28]
北京航空航天大学 [21]
力学研究所 [18]
清华大学 [1]
大连理工大学 [1]
长春光学精密机械与物... [1]
更多...
内容类型
会议论文 [44]
期刊论文 [24]
学位论文 [6]
发表日期
2021 [2]
2019 [6]
2018 [11]
2017 [7]
2016 [4]
2015 [3]
更多...
学科主题
Aircraft ... [16]
力学 [2]
Presented ... [1]
Presented ... [1]
材料工程 [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74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
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
收藏
  |  
浏览/下载:224/0
  |  
提交时间:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
Parametric study on wing-lambda-shock formation
会议论文
Virtual, Online, 10 August 2021 到 12 August 2021
作者:
Chainok S
;
Rungroch T
;
Chairach P
;
Prapamonthon P
;
Yooyen S
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2021/11/30
Shock
Supersonic flow
Transonic flow
Cooling Ability/Capacity and Exergy Penalty Analysis of Each Heat Sink of Modern Supersonic Aircraft
期刊论文
ENTROPY, 2019, 卷号: 21
作者:
Mao, Yu-Feng
;
Li, Yun-Ze
;
Wang, Ji-Xiang
;
Xiong, Kai
;
Li, Jia-Xin
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2019/12/30
aircraft
thermal management system
heat sink
cooling ability
cooling capacity
exergy
Transonic buffet control by rearward Buffet Breather on supercritical airfoil and wing
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 204-219
作者:
Jiang Runpei
;
Tian Yun
;
Liu Peiqing
收藏
  |  
浏览/下载:11/0
  |  
提交时间:2019/12/30
Aerodynamic drag
Airfoils
Angle of attack
Angle of attack indicators
Lift drag ratio
Merging
Navier Stokes equations
Quality control
Separation
Supersonic aircraft
Buffet condition
Lift coefficient
Lift to drag ratio
Pressure oscillation
Static aerodynamic characteristic
Supercritical airfoils
Transonic buffet
Unsteady reynolds-averaged navier-stokes methods
Wings
Effect of RANS Method on the Stall Onset Prediction by an Eigenvalue Approach
期刊论文
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2019, 卷号: 141
作者:
Xie, Zhe
;
Liu, Yangwei
;
Liu, Xiaohua
;
Lu, Lipeng
;
Sun, Xiaofeng
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Compressors
Computational fluid dynamics
Flow fields
Forecasting
NASA
Navier Stokes equations
Shear flow
Shear stress
Supersonic aircraft
Vortex flow
Wall function
Eigenvalue calculations
Flux difference splitting
Reynolds-averaged navier-stokes simulations
S-a turbulence models
Shear-stress transport
Spatial discretization schemes
Three dimensional flow field
Total variation diminishing
Eigenvalues and eigenfunctions
超声速民机声爆理论、预测和最小化方法概述
期刊论文
空气动力学学报, 2019, 卷号: 37, 页码: 646-654,645
作者:
兰世隆
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
声爆 预测 最小化 超声速民机 sonic boom prediction minimization supersonic aircraft
One-Equation Transition Model Based on Turbulent Kinetic Energy Transport [基于湍动能输运的一方程转捩模型]
期刊论文
Tuijin Jishu/Journal of Propulsion Technology, 2019, 卷号: 40, 页码: 741-749
作者:
Xu, J.-L.
;
Zhou, Y.
;
Qiao, L.
;
Xu, J.-K.
收藏
  |  
浏览/下载:16/0
  |  
提交时间:2019/12/30
Atmospheric thermodynamics
Boundary layer flow
Boundary layers
Computational fluid dynamics
Kinetic energy
Kinetics
Plates (structural components)
Supersonic aircraft
Turbulence models
Turbulent flow
Compressibility correction
Compressible boundary layers
High-fidelity
Laminar and turbulent flow
Separation-bubble transition
Transition model
Transition phenomenon
Turbulent kinetic energy
Transport properties
Dynamic modal analysis of circular-arc airfoil transonic flow [圆弧翼型跨声速流动的动态模态分析]
期刊论文
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2019, 卷号: 45, 页码: 1026-1032
作者:
Hu, W.
;
Yu, J.
;
Liu, H.
;
Yan, C.
收藏
  |  
浏览/下载:7/0
  |  
提交时间:2019/12/30
Aircraft manufacture
Airfoils
Airframes
Flow fields
Hypersonic aerodynamics
Modal analysis
Shock waves
Supersonic aircraft
Transonic aerodynamics
Transonic flow
Wave effects
Characteristic frequencies
Circular arc
Dynamic modal analysis
Dynamic mode decompositions
Flow field reconstruction
Frequency characteristic
Pressure fluctuation
Self-oscillations
Oscillating flow
化学非平衡对钝体绕流激波脱体距离影响的数值分析
学位论文
北京: 中国科学院大学, 2018
作者:
桂志宏
收藏
  |  
浏览/下载:107/0
  |  
提交时间:2018/05/29
钝体绕流
热化学非平衡
激波脱体距离
Cfd模拟
全乘波背部进气高超声速飞机新概念构型研究
学位论文
北京: 中国科学院大学, 2018
作者:
肖尧
收藏
  |  
浏览/下载:127/0
  |  
提交时间:2018/05/24
高超声速飞行器
乘波体
背部进气布局
升阻比
气动设计与优化
©版权所有 ©2017 CSpace - Powered by
CSpace