云南高校图书馆联盟文献共享服务平台- SCRAMJET

SCRAMJET: 作品数：63被引量：197H指数：7; 导出分析报告; 相关领域：航空宇航科学技术更多>>; 相关作者：乐嘉陵徐惊雷吴颖川王兰郑忠华更多>>; 相关机构：南京航空航天大学中国空气动力研究与发展中心中国科学技术大学哈尔滨工业大学更多>>; 相关期刊：《Theoretical & Applied Mechanics Letters》《Journal of Wuhan University of Technology(Materials Science)》《Chinese Journal of Mechanical Engineering》《Science Bulletin》更多>>; 相关基金：国家自然科学基金国家高技术研究发展计划国家重点基础研究发展计划航天科技创新基金更多>>

Data-driven surrogate modeling and optimization of supercritical jet into supersonic crossflow: 《Chinese Journal of Aeronautics》2024年第12期139-155,共17页Siyu DING Longfei WANG Qingzhou LU Xingjian WANG; supported by the Science Center for Gas Turbine Project,China(No.P2022-B-II-020-001);the National Natural Science Foundation of China(No.52276123).; For the design and optimization of advanced aero-engines,the prohibitively computational resources required for numerical simulations pose a significant challenge,due to the extensive exploration of design parameters ...; 关键词：Reduced-Order Model(ROM) SUPERCRITICAL Jet in crossflow SCRAMJET Uncertainty quantification Pareto-optimal frontier

A deep learning approach for velocity field prediction in a scramjet isolator from Schlieren images被引量：1: 《Chinese Journal of Aeronautics》2023年第11期58-70,共13页Chen KONG Ziao WANG Yunfei LI Juntao CHANG; supported by the National Natural Science Foundation of China(No.52125603).; Accurate measurements of physical parameters in a scramjet isolator are very important to promote the design and optimization of the isolator and even the scramjet.In a ground experiment,limited by the inherent charac...; 关键词：Data-driven model Deep learning Neural networks Scramjet isolator Velocity field prediction

Flamelet-like models applied in scramjet combustors:A state of art and prospect被引量：1: 《Chinese Journal of Aeronautics》2023年第10期24-43,共20页Tao TANG Zhenguo WANG Yuhui HUANG Mingbo SUN Hongbo WANG Guoyan ZHAO Jiangfei YU; the National Natural Science Foundation of China(Nos.12002381 and 11925207);the Science and Technology Foundation of State Key Laboratory,China(No.6142703200311);the Scientific Research Plan of National University of Defense Technology in 2019,China(No.ZK19-02).; Developing supersonic combustion models with efficiency,accuracy and practicality is important foundation to deeply understand the complex combustion processes in scramjet engines.Characterized by efficiency and intui...; 关键词：Combustion model Flamelet-like model Model improvements Supersonic combustion SCRAMJET

MCGA-assisted ignition process and flame propagation of a scramjet at Mach 2.0被引量：2: 《Chinese Journal of Aeronautics》2023年第7期378-387,共10页Tiangang LUO Jiajian ZHU Mingbo SUN Rong FENG Yifu TIAN Qinyuan LI Minggang WAN Yongchao SUN; supported by the National Natural Science Foundation of China(Nos.12172379,11925207,and 91741205);the Foundation for Outstanding Young Scholars of National University of Defense Technology,China.; The ignition process and flame propagation with ethylene fuel in cavity-stabilized scramjet by a Multi-Channel Gliding Arc(MCGA)at Mach 2.0 were investigated.Effects of equivalence ratios on the MCGA-assisted ignition...; 关键词：Cavity Ignition process Multi-Channel Gliding Arc(MCGA) SCRAMJET Supersonic flow

A power and thermal management system for long endurance hypersonic vehicle被引量：5: 《Chinese Journal of Aeronautics》2023年第2期29-40,共12页Liang GUO Liping PANG Xiaodong YANG Jingquan ZHAO Desheng MA; Due to the pneumatic heating and combustion effect,the scramjet engine of hypersonic vehicle faces high temperature challenge.It is necessary to comprehensively consider its thermal management and power generation tog...; 关键词：Fuel vapor turbine Hypersonic vehicle Power and thermal management system SCRAMJET Supercritical carbon dioxide

Experimental study on flow excursion instability of supercritical hydrocarbon fuel in scramjet regenerative cooling parallel channels被引量：2: 《Chinese Journal of Aeronautics》2023年第1期201-215,共15页Xiaoyong LIU Zhuqiang YANG Ruipu MIAO Feng LIU Shujun ZHAO Qincheng BI; co-supported by the Open Fund of Key Laboratory of Power Research of China(No.2017-Ⅲ-0005-0029);the National Natural Science Foundation of China(No.51776167).; Flow instability of supercritical hydrocarbon fuel is a crucial issue in scramjet regenerative cooling structure. In this study, flow excursion instability and flow distribution in parallel tubes were experimentally s...; 关键词：Flow distribution Ledinegg instability Onset of flow excursion Parallel channels Regenerative cooling SCRAMJET Supercritical flow

Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets被引量：4: 《Chinese Journal of Aeronautics》2023年第1期216-230,共15页Guangwei MA Mingbo SUN Guoyan ZHAO Changhai LIANG Hongbo WANG Jiangfei YU; supported by the National Natural Science Foundation of China(Nos.11925207,12002381);the Scientific Research Plan of National University of Defense Technology in 2019,China(No.ZK19-02);the Postgraduate Scientific Research Innovation Project of Hunan Province,China(No.CX20200084);the Equipment Pre-research Foundation of Key Laboratory,China(No.6142703200311)。; The asymmetric separation has a crucial effect on the performance of the scramjet.In this study,the asymmetric separation and combustion in both rectangular and circular scramjets are investigated numerically,and the ...; 关键词：Asymmetric phenomenon CAVITY Combustion Injection scheme SCRAMJET SUPERSONIC

Research progress on solid-fueled Scramjet被引量：7: 《Chinese Journal of Aeronautics》2022年第1期398-415,共18页Xiang ZHAO Zhixun XIA Likun MA Chaolong LI Chuanbo FANG Benveniste NATAN Alon GANY; supported by the China Scholarship Council and the National Natural Science Foundation of China(Nos.2020JJ4665,51706241).; The solid-fueled Scramjet is an interesting option for supersonic combustion ramjet.It shows significant advantages such as simple fuel supply and compactness,avoiding the complex system of tanks and pipelines that en...; 关键词：Combustor performance Flame stabilization SELF-IGNITION Solid-fueled Scramjet Supersonic combustion ramjet

Scaling effects on combustion modes in a single-side expansion kerosene-fueled scramjet combustor被引量：3: 《Chinese Journal of Aeronautics》2021年第5期684-690,共7页Fan LI Mingbo SUN Jiajian ZHU Zun CAI Hongbo WANG Yanxiang ZHANG Yongchao SUN; supported by the National Natural Science Foundation of China(Nos.11925207,11902353 and 91741205);the Foundation of Innovation-oriented Province Construction of Hunan(No.2019RS2028)。; The combustion modes in two different scramjet combustors with the mass flow rates of 1.8 kg/s and 3.6 kg/s are experimentally investigated to explore the scaling effects on supersonic combustion with a Mach number 2....; 关键词：Cavity COMBUSTION Combustion stabilized mode Scaling effect SCRAMJET SUPERSONIC

Criteria for hypersonic airbreathing propulsion and its experimental verification被引量：18: 《Chinese Journal of Aeronautics》2021年第3期94-104,共11页Zonglin JIANG Zijian ZHANG Yunfeng LIU Chun WANG Changtong LUO; supported by the National Natural Science Foundation of China (No. 11532014)。; Hypersonic airbreathing propulsion is one of the top techniques for future aerospace flight, but there are still no practical engines after seventy years’ development. Two critical issues are identified to be the bar...; 关键词：Concept demonstration Hypersonic propulsion Oblique detonation engine SCRAMJET Shock wave Supersonic combustion Wind tunnel test

高级检索 检索式检索

时间限定

期刊范围

学科限定全选

高级检索 检索式检索

时间限定

期刊范围

学科限定全选

SCRAMJET

检索结果分析

下载全文

高级检索检索式检索

时间限定

期刊范围

学科限定全选

高级检索 检索式检索

时间限定

期刊范围

学科限定全选

SCRAMJET

检索结果分析

下载全文

用户登录

高级检索检索式检索