IMECH-IR
(本次检索基于用户作品认领结果)

浏览/检索结果: 共18条,第1-10条 帮助

限定条件            
已选(0)清除 条数/页:   排序方式:
超声速三维进气道内激波干扰的研究 期刊论文
推进技术, 2017, 期号: 12, 页码: 6
作者:  项高翔;  王春;  汪运鹏;  姜宗林
Adobe PDF(1393Kb)  |  收藏  |  浏览/下载:461/92  |  提交时间:2017/12/22
高超声速流动  箱式进气道  侧壁压缩进气道  波系结构  流场区域  
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
作者:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1080Kb)  |  收藏  |  浏览/下载:511/125  |  提交时间:2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
JF12长实验时间激波风洞10°尖锥气动力实验研究 期刊论文
气体物理, 2017, 卷号: 2, 期号: 02, 页码: 1-7
作者:  刘云峰;  汪运鹏;  苑朝凯;  罗长童;  姜宗林
Adobe PDF(2256Kb)  |  收藏  |  浏览/下载:309/55  |  提交时间:2017/12/22
Jf12长实验时间激波风洞  高超声速气动力特性  10°尖锥标模  真实气体效应  
Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(6096Kb)  |  收藏  |  浏览/下载:302/86  |  提交时间:2018/01/16
激波风洞应变天平测力技术研究 会议论文
第九届全国流体力学学术会议, 中国江苏南京, 2016-10-20
作者:  汪运鹏;  刘云峰;  姜宗林
Adobe PDF(115Kb)  |  收藏  |  浏览/下载:309/78  |  提交时间:2017/09/27
激波风洞  长试验时间  气动力测量  应变天平  
Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
作者:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(764Kb)  |  收藏  |  浏览/下载:329/89  |  提交时间:2017/09/19
Force measurement using strain-gauge balance in a shock tunnel with long test duration 期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2016, 卷号: 87, 期号: 5, 页码: 55108
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
Adobe PDF(6592Kb)  |  收藏  |  浏览/下载:315/87  |  提交时间:2016/09/14
Design of a pulse-type strain gauge balance for a long-test-duration hypersonic shock tunnel 期刊论文
SHOCK WAVES, 2016, 卷号: 26, 期号: 6, 页码: 835-844
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
Adobe PDF(2538Kb)  |  收藏  |  浏览/下载:380/82  |  提交时间:2016/12/08
Hypersonic Shock Tunnel  Force Measurement  Strain Gauge Balance  
Starting Process in a Large-Scale Shock Tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
作者:  Wang YP;  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(764Kb)  |  收藏  |  浏览/下载:344/95  |  提交时间:2016/06/28
Force measurement in a shock tunnel with 100 milliseconds test duration 会议论文
34th AIAA Applied Aerodynamics Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(6592Kb)  |  收藏  |  浏览/下载:302/78  |  提交时间:2017/05/05
Aerodynamic Forces  Chinese Academy Of Sciences  Different Structure  Digital Filtering  Large  Scale Modeling  Low  Frequency Vibration  Strain Gauge Balances  Strain Gauge Sensors