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杨乾锁 [19]
彭志敏 [10]
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A high-precision NO
x
chemiluminescence sensor of sub-ppb-level based on air-fed ozoniser and flow-restricting capillary
期刊论文
INTERNATIONAL JOURNAL OF ENVIRONMENTAL ANALYTICAL CHEMISTRY, 2024, 页码: 16
Authors:
Zhang M(张猛)
;
Peng, ZhiMin
;
Yang QS(杨乾锁)
;
Ding, YanJun
;
Du, YanJun
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View/Download:17/0
  |  
Submit date:2024/05/14
Chemiluminescence
air-fed ozoniser
flow-restricting capillary
NOx gas sensor
注入光有限相干性对衰荡腔测试方法的影响及求解衰荡时间的强度积分法
期刊论文
物理学报, 2023, 卷号: 72, 期号: 18, 页码: 217-225
Authors:
黄知秋
;
张猛
;
彭志敏
;
王振
;
杨乾锁
Adobe PDF(4990Kb)
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View/Download:128/26
  |  
Submit date:2023/11/28
cavity ring-down spectroscopy
light coherence
ring-down time
intensity integration
Heat transfer effects on multiphase Richtmyer-Meshkov instability of dense gas-particle flow
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 53339
Authors:
Si YM(司英明)
;
Li, Shuai
;
Chen, Qian
;
Meng, Baoqing
;
Wang C(王春)
;
Tian, Baolin
Adobe PDF(5207Kb)
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  |  
Submit date:2023/07/17
基于化学发光法的高纯气体中ppb量级NO_x浓度测量
期刊论文
物理学报, 2022, 卷号: 71, 期号: 13, 页码: 374-382
Authors:
张猛
;
彭志敏
;
杨乾锁
;
丁艳军
;
杜艳君
Adobe PDF(1885Kb)
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View/Download:153/51
  |  
Submit date:2022/08/11
化学发光
高纯气体
痕量气体
淬灭
Reduction of surface friction drag in scramjet engine by boundary layer combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:
Xue, Rui
;
Zheng, Xing
;
Yue LJ(岳连捷)
;
Zhang, Qian
;
He, Xin
;
Yang, Jing
;
Weng, Chao
;
Li, Zhihao
Adobe PDF(5483Kb)
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  |  
Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
一种高超声速高焓地面模拟设备的加热器点火器
专利
发明专利. 一种高超声速高焓地面模拟设备的加热器点火器, 专利号: ZL201610864921.1, 申请日期: 2016-09-29, 授权日期: 2018-11-09
Inventors:
顾洪斌
;
张新宇
;
林建民
;
高占彪
;
钱大兴
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  |  
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View/Download:204/35
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Submit date:2018/12/05
一种高超声速高焓地面模拟设备的燃料室头部
专利
发明专利. 一种高超声速高焓地面模拟设备的燃料室头部, 专利号: ZL201510209803.2, 申请日期: 2015-04-28, 授权日期: 2017-09-26
Inventors:
顾洪斌
;
张新宇
;
李东霞
;
邢云绯
;
仲峰泉
;
林建民
;
高占彪
;
钱大兴
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  |  
Adobe PDF(548Kb)
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View/Download:315/52
  |  
Submit date:2017/10/13
Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds
会议论文
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russia, September 7, 2014 - September 12, 2014
Authors:
Qian W
;
Yang GW(杨国伟)
;
Zheng GN(郑冠男)
;
Zhang GJ
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  |  
Adobe PDF(1159Kb)
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Submit date:2017/05/27
All-movable Horizontal Tail
Flutter Boundaries
Overload Factors
Structure Dynamics
Transonic Flutter
Transonic Speed
Wind Tunnel Tests
Wind-tunnel Testing
基于压缩气体驱动的高速列车模型加速装置
专利
发明专利. 基于压缩气体驱动的高速列车模型加速装置, 专利号: ZL2011103988086, 申请日期: 2011-12-05, 授权日期: 2013-12-23
Inventors:
杨乾锁
;
杨国伟
Adobe PDF(423Kb)
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View/Download:627/197
  |  
Submit date:2013/12/23
一种用于高速列车动模型实验平台的减速装置
专利
发明专利. 一种用于高速列车动模型实验平台的减速装置, 专利号: ZL201220577232X, 申请日期: 2012-11-05, 授权日期: 2013-04-03
Inventors:
杨乾锁
;
杨国伟
Adobe PDF(232Kb)
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View/Download:897/147
  |  
Submit date:2013/04/03