المؤلفون: Chen LH(陈立红), Yue LJ(岳连捷), Zhang XY(张新宇), Xiao YB(肖雅彬)

المصدر: 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.

مصطلحات موضوعية: Hypersonic speed, Engineering, geography, geography.geographical_feature_category, business.industry, Rotational symmetry, Mechanics, Structural engineering, Inlet, symbols.namesake, Mach number, symbols, Supersonic speed, Point (geometry), Tube (container), business, Contraction ratio

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::6fb7799ce2be692a170f1ba3e3c29bd3
https://doi.org/10.2514/6.2012-5978

المؤلفون: Chen TY(陈同银), Zhang XY(张新宇), Fan XJ(范学军), Chen LH(陈立红), Zhong FQ(仲峰泉)

المصدر: 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.

مصطلحات موضوعية: Engineering, Internal flow, business.industry, Structural engineering, Mechanics, Coolant, symbols.namesake, Mach number, Heat transfer, Total air temperature, Combustor, symbols, Supersonic speed, Scramjet, business

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::0e9b9aea63e926c4f91f0e90bf0508dd
https://doi.org/10.2514/6.2012-3926

المؤلفون: Gu HB(顾洪斌), Chen LH(陈立红), Gu SL(顾声龙), Zhang XY(张新宇), Li Z(李智), Li F(李飞)

المصدر: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.

مصطلحات موضوعية: Physics::Fluid Dynamics, Jet (fluid), Chemistry, Astrophysics::High Energy Astrophysical Phenomena, Excited state, Turbulence kinetic energy, Combustor, High Energy Physics::Experiment, Supersonic speed, Static pressure, Atomic physics, Combustion, Choked flow

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::7e29d7fdc05f83e913fbfbdc302bbbd9
https://doi.org/10.2514/6.2011-2326

المؤلفون: Yue LJ(岳连捷), Zhang XY(张新宇), Chen LH(陈立红), Xiang AY(向安宇), Xiao YB(肖雅彬)

المصدر: 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference.

مصطلحات موضوعية: geography, geography.geographical_feature_category, Materials science, Shock (fluid dynamics), business.industry, Flow (psychology), Unstart, Mechanics, Structural engineering, Inlet, Flow separation, Boundary layer, Scramjet, Total pressure, business

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::335581ed71a7f51f7bc400597b8c4a0f
https://doi.org/10.2514/6.2006-8141

المؤلفون: Zhang SH(张少华), Yu XL(余西龙), Chen LH(陈立红), Zhang XY(张新宇), Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.

مصطلحات موضوعية: Premixed Flames, Plasma, Methane, Mixtures, Planar Laser Induced Fluorescence, Laser Diagnostics, Flame Velocities, Emission Spectra, Dielectric Barrier Discharge, 流体力学::空气动力学, PRESSURE, JET, Physics, Multidisciplinary, Q3, astrophysical plasma, laminar flow, space plasmas, luminescence, ion density, plasmoids, plasma applications, 泊肃叶流, 大旋涡, vortex, 旋涡运动, laminar boundary layers, vortices, enstrophy, plasma vortices

Relation: CHINESE PHYSICS LETTERS; Zhang SH,Yu XL,Chen LH,et al. Laser Diagnostics of Combustion Enhancement on a CH4/Air Bunsen Flame by Dielectric Barrier Discharge[J]. CHINESE PHYSICS LETTERS,2013,30(8):085203/1-085203/4.; http://dspace.imech.ac.cn/handle/311007/47447; http://dx.doi.org/10.1088/0256-307X/30/8/085203

الاتاحة: http://dspace.imech.ac.cn/handle/311007/47447
https://doi.org/10.1088/0256-307X/30/8/085203

المؤلفون: Li F(李飞), Yu XL(余西龙), Tong YG(仝颖刚), Shen Y(沈岩), Chen J(陈健), Chen LH(陈立红), Zhang XY(张新宇), Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.

مصطلحات موضوعية: Scramjet, Kerosene Fuel, Plasma Torch, Ignition, 流体力学, 二类, plasma jets, jets, plasma, plasma arcs, plasma discharges, 着火, electric ignition, glow plugs, reignition, 灼烧

Relation: AEROSPACE SCIENCE AND TECHNOLOGY; Li F,Yu XL,Tong YG,et al. Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2013,28(1):72-78.; http://dspace.imech.ac.cn/handle/311007/47336; http://www.sciencedirect.com/science/article/pii/S1270963812001551

الاتاحة: http://dspace.imech.ac.cn/handle/311007/47336
http://www.sciencedirect.com/science/article/pii/S1270963812001551

المؤلفون: Dang GX(党国鑫), Zhong FQ(仲峰泉), Chen LH(陈立红), Zhang XY(张新宇), Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.

مصطلحات موضوعية: 流体力学, 二类/Q2

Relation: SCIENCE CHINA-TECHNOLOGICAL SCIENCES; Dang GX,Zhong FQ,Chen LH,et al. Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions[J]. SCIENCE CHINA-TECHNOLOGICAL SCIENCES,2013,56(2):416-422.; http://dspace.imech.ac.cn/handle/311007/46937; http://dx.doi.org/10.1007/s11431-012-5075-3

الاتاحة: http://dspace.imech.ac.cn/handle/311007/46937
https://doi.org/10.1007/s11431-012-5075-3

المؤلفون: Gu HB(顾洪斌), Chen LH(陈立红), Zhang XY(张新宇), 顾洪斌

مصطلحات موضوعية: Scramjet, Combustor, Cavity, Performance, 固体力学::弹性力学与塑性力学, SUPERSONIC COMBUSTORS, FUEL-INJECTION, FLAME STABILIZATION, FLOW, MECHANISM, Science & Technology - Other Topics, [空]腔, competence, incompetence, mental, mental competence

Relation: CHINESE SCIENCE BULLETIN; Gu HB,Chen LH,Zhang XY. Experimental investigation on the cavity-based scramjet model[J]. CHINESE SCIENCE BULLETIN,2009,54(16):2794-2799.; http://dspace.imech.ac.cn/handle/311007/26508

الاتاحة: http://dspace.imech.ac.cn/handle/311007/26508
https://doi.org/10.1007/s11434-009-0460-4

المؤلفون: Tian XD, Chen LH(陈立红), Gu HB(顾洪斌), Liu C, Cheng LW, Chang XY(张新宇), Chen, Lihong (lhchen@imech.ac.cn)

Relation: Tian XD,Chen LH,Gu HB,et al. Experimental study of combustion oscillations in a dual-mode scramjet[C]. 见:20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015. 2015; http://dspace.imech.ac.cn/handle/311007/60702

الاتاحة: http://dspace.imech.ac.cn/handle/311007/60702

المؤلفون: Chen Q(陈强), Chen LH(陈立红), Gu HB(顾洪斌), Zhang XY(张新宇), Wang P

مصطلحات موضوعية: Combustion Mode, Scramjet, Artificial Neural Network

Relation: PROCEDIA ENGINEERING; Chen Q,Chen LH,Gu HB,et al. Study on Judgment Method of Combustion Mode on Dual-mode Scramjet[C]. 见:7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013. Taiwan, China. MAY 23-26, 2013.http://dx.doi.org/10.1016/j.proeng.2013.12.014; http://dspace.imech.ac.cn/handle/311007/48334; http://dx.doi.org/10.1016/j.proeng.2013.12.014

الاتاحة: http://dspace.imech.ac.cn/handle/311007/48334
https://doi.org/10.1016/j.proeng.2013.12.014

المؤلفون: Zhong FQ(仲峰泉), Chen LH(陈立红), Chang XY(张新宇), 仲峰泉

Relation: 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012; Zhong FQ,Chen LH,Chang XY. Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor[C]. 见:18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. Tours, France. SEP 24-28, 2012; http://dspace.imech.ac.cn/handle/311007/48283

الاتاحة: http://dspace.imech.ac.cn/handle/311007/48283

المؤلفون: Xiao YB(肖雅彬), Yue LJ(岳连捷), Chen LH(陈立红), Zhang XY(张新宇), 肖雅彬

Relation: 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012; Xiao YB,Yue LJ,Chen LH,et al. Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition[C]. 见:18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. Tours, France. SEP 24-28, 2012; http://dspace.imech.ac.cn/handle/311007/48282

الاتاحة: http://dspace.imech.ac.cn/handle/311007/48282

المؤلفون: Tian L(田璐), Chen LH(陈立红), Chen Q(陈强), Li F(李飞), Zhang XY(张新宇), 田璐

Relation: 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012; http://dspace.imech.ac.cn/handle/311007/48284

الاتاحة: http://dspace.imech.ac.cn/handle/311007/48284
http://arc.aiaa.org/doi/abs/10.2514/6.2012-5833

المؤلفون: 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), 仲峰泉

Relation: 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012; Zhong FQ,Chen TY,Fan XJ,et al. Three-Dimensional heat transfer analysis and optimized design of actively cooled strut for scramjet applications[C]. 见:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012. Atlanta, GA, United states. JUL 30-AUG 01, 2012; http://dspace.imech.ac.cn/handle/311007/48276

الاتاحة: http://dspace.imech.ac.cn/handle/311007/48276

المؤلفون: Zhong FQ(仲峰泉), Wang X(王曦), Chen LH(陈立红), 张新宇(Chang XY)

مصطلحات موضوعية: 交叉与边缘领域的力学::物理力学

Relation: 仲峰泉;王曦;陈立红;张新宇(Chang XY). Numerical Study of ConvectiveHeat Transfer of Supersonic Combustor[C].2012.; Zhong FQ,Wang X,Chen LH,et al. Numerical Study of Convective Heat Transfer of Supersonic Combustor[C]. 见:The Asian Joint Conference on Propulsion and Power 2012 （2012年亚洲推进与动力会议 ）. 陕西、西安. 2012-03-01~2012-03-03.http://www.meeting.edu.cn/meeting/mediaAction!mediaDetail.action?id=10779; http://dspace.imech.ac.cn/handle/311007/46804; http://www.meeting.edu.cn/meeting/mediaAction!mediaDetail.action?id=10779

الاتاحة: http://dspace.imech.ac.cn/handle/311007/46804
http://www.meeting.edu.cn/meeting/mediaAction!mediaDetail.action?id=10779

المؤلفون: 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), 李飞

Relation: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011; Li F,Yu XL,Gu HB,et al. Measurement of temperature, velocity and water vapor concentration in a scramjet combustor based on nearinfrared diode laser absorption[C]. 见:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco, CA, United states. APR 11-14, 2011.http://dx.doi.org/10.2514/6.2011-2214; http://dspace.imech.ac.cn/handle/311007/48286; http://dx.doi.org/10.2514/6.2011-2214

الاتاحة: http://dspace.imech.ac.cn/handle/311007/48286
https://doi.org/10.2514/6.2011-2214

المؤلفون: Wan T(万田), Chen LH(陈立红), Wang J(王晶), Fan XJ(范学军), Zhang XY(张新宇), Wan, TA (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.

Relation: PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2; Wan T,Chen LH,Wang J,et al. CFD Simulation of Kerosene-Fueled Supersonic Combustion Ramjet Combustor Experiments[C]. 见:Asia-Pacific International Symposium on Aerospace Technology. Xian, PEOPLES R CHINA. SEP 13-15, 2010; http://dspace.imech.ac.cn/handle/311007/58875

الاتاحة: http://dspace.imech.ac.cn/handle/311007/58875

المؤلفون: Zhang XY(张新宇), Chen LH(陈立红), Gu HB(顾洪斌), Yu G(俞刚), 张新宇

مصطلحات موضوعية: 力学

Relation: Shock Waves; Zhang XY,Chen LH,Gu HB,et al. Experimental Studies on Model Scramjet in a Mach 6 High Enthalpy Free-Jet Wind Tunnel[C]. 见:The 24th International Symposium on Shock Waves. Beijing. 2004-07-11.http://dx.doi.org/10.1007/978-3-540-27009-6_135; http://dspace.imech.ac.cn/handle/311007/13771; http://dx.doi.org/10.1007/978-3-540-27009-6_135

الاتاحة: http://dspace.imech.ac.cn/handle/311007/13771
https://doi.org/10.1007/978-3-540-27009-6_135