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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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State Key ... [7]
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张新宇 [7]
陈立红 [7]
李飞 [5]
顾洪斌 [4]
顾声龙 [3]
卫喆 [2]
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Indexed By:EI
Creator:陈立红
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Document Type:会议论文
Community:高温气体动力学国家重点实验室
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Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:
Xiao YB(肖雅彬)
;
Yue LJ(岳连捷)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Xiao YB(肖雅彬)
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Submit date:2014/02/24
Three-Dimensional heat transfer analysis and optimized design of actively cooled strut for scramjet applications
会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:
Zhong FQ(仲峰泉)
;
Chen TY(陈同银)
;
Fan XJ(范学军)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Zhong FQ(仲峰泉)
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Submit date:2014/02/24
Modeling and measurements of heat release distributions in dual-mode scramjet combustor
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:
Tian L(田璐)
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Tian L(田璐)
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Submit date:2014/02/24
Measurement of temperature, velocity and water vapor concentration in a scramjet combustor based on nearinfrared diode laser absorption
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Gu HB(顾洪斌)
;
Li Z(李智)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Li F(李飞)
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  |  
Submit date:2014/02/24
Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Gu HB(顾洪斌)
;
Li Z(李智)
;
Li F(李飞)
;
Chen LH(陈立红)
;
Gu SL(顾声龙)
;
Zhang XY(张新宇)
;
Gu HB(顾洪斌)
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  |  
Adobe PDF(242Kb)
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Submit date:2014/02/24
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
Flow-field of the excited jet and mixing in the supersonic flow
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:
Gu SL(顾声龙)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Li F(李飞)
;
Wei Z(卫喆)
;
Chang XY(张新宇)
;
Gu, S. (gushenglong@imech.ac.cn)
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Submit date:2017/07/14
Different Frequency
Gas Sampling
Hartmann
Jet Devices
Large-scale Structure
Planar Laser
Shear Layer
Total-pressure Loss