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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yu, Jianyi
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View/Download:15/0
  |  
Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
激波风洞两级入轨飞行器纵向级间分离试验技术
期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors:
王粤
;
汪运鹏
;
姜宗林
Adobe PDF(6797Kb)
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View/Download:321/32
  |  
Submit date:2022/12/01
两级入轨
轨迹捕获
激波风洞
多体分离
动态试验
试验技术
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:
Yuan CK(苑朝凯)
;
Meng FZ(孟凡钊)
;
Liu, Xu
;
Liu YF(刘云峰)
;
Lian H(连欢)
;
Liu, Yingzheng
;
Peng, Di
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  |  
View/Download:40/0
  |  
Submit date:2023/07/17
Temperature-sensitive paint
Heat flux
Conjugate gradient method
Air-breathing hypersonic vehicle
Inverse heat conduction problem
Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
Authors:
Peng J(彭俊)
;
Li S(李帅)
;
Yang F(杨帆)
;
Lin MY(林明月)
;
Han GL(韩桂来)
;
Hu ZM(胡宗民)
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View/Download:52/0
  |  
Submit date:2023/04/20
Shock interactions
Transitional configuration
Aerodynamic heating
Shear layer
Mach interaction
Hypersonic shock wave and turbulent boundary layer interaction in a sharp cone/flare model
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 80-95
Authors:
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Lai, Jiang
;
Sun, Dong
;
Yuan, Xianxu
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View/Download:42/0
  |  
Submit date:2023/04/20
Shock wave
Hypersonic turbulent
boundary layer
Heat transfer
Skin friction decomposition
Direct numerical simulation
On the accuracy of two temperature models for hypersonic nonequilibrium flow
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 2, 页码: 122193
Authors:
Wang XY(王小永)
;
Hong QZ(洪启臻)
;
Hu Y(胡远)
;
Sun QH(孙泉华)
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View/Download:49/0
  |  
Submit date:2023/04/20
Nonequilibrium flow
Two temperature model
Quasi classical trajectory
Non Boltzmann effect
Vibration dissociation coupling effect
高速弹丸诱导斜爆轰激波结构实验研究
期刊论文
力学学报, 2023, 卷号: 55, 期号: 02, 页码: 309-317
Authors:
尚甲豪
;
胡国暾
;
汪球
;
王业军
;
张坤
;
项高翔
;
赵伟
;
魏炳忱
Adobe PDF(1612Kb)
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View/Download:187/38
  |  
Submit date:2023/03/16
斜爆轰
超声速燃烧
激波诱导燃烧
斜爆轰波
二级轻气炮
一种并联两级入轨飞行器纵向分离方案的数值研究
期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
Authors:
王粤
;
汪运鹏
;
王春
;
姜宗林
Adobe PDF(4901Kb)
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View/Download:538/78
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Submit date:2022/07/11
两级入轨
高超声速
纵向分离
气动干扰
非定常流动
基于主动射流控制的高超声速进气道再起动性能研究(英文)
期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:
靳一超
;
姚卫
Adobe PDF(1844Kb)
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View/Download:127/33
  |  
Submit date:2023/02/09
高超声速进气道
不起动
再起动
主动射流
流动控制
翼反角对高压捕获翼构型亚声速气动特性影响分析研究
期刊论文
力学学报, 2022, 卷号: 54, 期号: 10, 页码: 2760-2772
Authors:
常思源
;
肖尧
;
李广利
;
田中伟
;
崔凯
Adobe PDF(1833Kb)
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View/Download:226/53
  |  
Submit date:2022/11/07