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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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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
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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
激波风洞高低压段钢膜片破裂特性研究
期刊论文
力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1747-1757
Authors:
聂少军
;
汪运鹏
;
薛晓鹏
;
姜宗林
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Submit date:2021/11/12
激波风洞
主膜片
爆轰驱动
破裂特性
数值模拟
基于变分法的冷却结构优化设计与分析方法
期刊论文
推进技术, 2020, 卷号: 41, 期号: 05, 页码: 1121-1129
Authors:
李轩
;
陆阳
;
吴坤
;
范学军
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Submit date:2020/07/15
变分
冷却
优化
自适应
多目标
Study of coupled effect of impingement jet cooling of kerosene with solid structure
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2019, 卷号: 62, 期号: 11, 页码: 2021-2028
Authors:
Du MM(杜蒙蒙)
;
Zhong FQ(仲峰泉)
;
Xing YF(邢云绯)
;
Zhang XY(张新宇)
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Submit date:2020/03/21
impingement jet cooling
hydrocarbon fuel
heat transfer enhancement
fluid-solid coupling
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
升阻比对可重复使用运载器爬升特性影响
期刊论文
中国科学:技术科学, 2019, 期号: 08, 页码: 891-900
Authors:
崔凯
;
徐应洲
;
李广利
;
肖尧
;
王浩祥
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Submit date:2019/09/12
可重复使用运载器
水平发射
两级入轨
弹道分析
升阻比
页岩气开采中的若干力学前沿问题
期刊论文
力学进展, 2019, 卷号: 49, 期号: 00, 页码: 1-236
Authors:
刘曰武
;
高大鹏
;
李奇
;
万义钊
;
段文杰
;
曾霞光
;
李明耀
;
苏业旺
;
范永波
;
李世海
;
鲁晓兵
;
周东
;
陈伟民
;
傅一钦
;
姜春晖
;
侯绍继
;
潘利生
;
魏小林
;
胡志明
;
端祥刚
;
高树生
;
沈瑞
;
常进
;
李晓雁
;
柳占立
;
魏宇杰
;
郑哲敏
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Submit date:2019/09/12
页岩气
压裂
力学性质
数值模拟
监测技术
渗流
An efficient unstructured WENO method for supersonic reactive flows
期刊论文
ACTA MECHANICA SINICA, 2018, 卷号: 34, 期号: 4, 页码: 623-631
Authors:
Zhao WG
;
Zheng HW(郑洪伟)
;
Liu FJ
;
Shi XT
;
Gao J
;
Hu N
;
Lv M
;
Chen SC
;
Zhao HD
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Submit date:2018/10/30
Supersonic reactive flows
Adaptive splitting scheme
Unstructured grids
WENO reconstruction
结构振动对大型激波风洞气动力测量的干扰
期刊论文
力学学报, 2016, 卷号: 48, 期号: 1, 页码: 102-110
Authors:
孟宝清
;
韩桂来
;
姜宗林
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Submit date:2016/03/01
Shock Tunnel
Aerodynamic Force Measurement
Vibration Interference
Theoretical Investigation
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:
Xing YF(邢云绯)
;
Zhong FQ(仲峰泉)
;
Li DX(李东霞)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel
Nozzle
Aerodynamic Heating
Convective Heat Transfer