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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)
浏览  |  Adobe PDF(764Kb)  |  收藏  |  浏览/下载：329/89  |  提交时间：2017/09/19
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.
浏览  |  Adobe PDF(764Kb)  |  收藏  |  浏览/下载：345/96  |  提交时间：2016/06/28
Role of wall temperature on shock train in a rectangular isolator 会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
作者:  Lu HB;  Wang D;  Chen X;  Yue LJ(岳连捷);  Ji, Feng (yuelj@imech.ac.cn)
浏览  |  Adobe PDF(560Kb)  |  收藏  |  浏览/下载：253/87  |  提交时间：2017/05/05
Aero  Heating  Dual Mechanisms  On Flow  Shock Train  Specific Heat Ratio  Total Pressure  Total Temperatures  Wall Temperatures  
轴对称激励射流特性研究 学位论文
硕士论文，北京: 中国科学院大学, 2016
作者:  闫继东
Adobe PDF(11959Kb)  |  收藏  |  浏览/下载：198/3  |  提交时间：2016/08/29
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
作者:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1162Kb)  |  收藏  |  浏览/下载：327/81  |  提交时间：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Development and calibration of detonation-driven high-enthalpy and hypersonic test facilities 图书章节
2016
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
浏览  |  Adobe PDF(883Kb)  |  收藏  |  浏览/下载：217/38  |  提交时间：2018/11/06
Heat Transfer and Mode Transition for Laser Ablation Subjected to Supersonic Airflow 期刊论文
CHINESE PHYSICS LETTERS, 2016, 卷号: 33, 期号: 1, 页码: 14201
作者:  Huang YH;  Song HW(宋宏伟);  Huang CG(黄晨光);  Song, HW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(669Kb)  |  收藏  |  浏览/下载：308/90  |  提交时间：2016/03/21
A quasi-one-dimensional model for hypersonic reactive flow along the stagnation streamline 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 期号: 6, 页码: 1517-1526
作者:  Chen S;  Sun QH(孙泉华)
浏览  |  Adobe PDF(1688Kb)  |  收藏  |  浏览/下载：239/70  |  提交时间：2017/04/26
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor 会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
作者:  Cheng D(程迪);  Wang J(王晶);  Gong J;  Lu Y(陆阳);  Yao W(姚卫);  Li L(李龙);  Fan XJ(范学军);  Fan, Xuejun (xfan@imech.ac.cn)
Adobe PDF(2131Kb)  |  收藏  |  浏览/下载：318/121  |  提交时间：2017/05/05
Equivalence Ratios  Heat Flux Distributions  Heat Transfer Characteristics  Scramjet  Supercritical Kerosenes  Supersonic Combustion  Supersonic Combustors  Total Temperatures