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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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Investigation for Effects of Jet Scale on Flame Stabilization in Scramjet Combustor
期刊论文
ENERGIES, 2022, 卷号: 15, 期号: 10, 页码: 16
Authors:
Li Z(李桢)
;
Gu HB(顾洪斌)
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Submit date:2022/07/18
scramjet combustor
direct-connect test
jet scale
flame stabilization
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
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
Performance of the fuel injector in supersonic combustor
会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:
Wei Z(卫喆)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Li F(李飞)
;
Gu SL(顾声龙)
;
Chang XY(张新宇)
;
Wei, Z. (weizhejiji@yahoo.com.cn)
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Submit date:2017/07/14
Concentration Profiles
Engine Design
Fuel Injectors
Fuel-air Mixing
Gas Sampling
Ramp Injector
Scramjet Combustors
Scramjet Test
Supersonic Combustors
Three-dimensional sidewall-compression scramjet inlet CFD simulation and experimental comparison
会议论文
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, United states, July 20, 2003 - July 23, 2003
Authors:
Chen F
;
Chen LH(陈立红)
;
Chang XY(张新宇)
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Submit date:2017/06/01
Compressible Navier-stokes
Computational Studies
Experimental Comparison
Experimental Investigations
Flow Charac-teristics
Hypersonic Propulsion Test Facility
Performance Parameters
Scramjet Inlets
Development of the facility for model scramjet testing
会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
Authors:
Chang XY(张新宇)
;
Chen LH(陈立红)
;
Yu G(俞刚)
;
Qian DX(钱大兴)
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Submit date:2017/06/01
Chinese Academy Of Sciences
Enthalpy Flow
Hypersonic Propulsion Test Facility
Performance Tests
Scramjet Testing
Supersonic Combustion
Total Pressure
Total Temperatures