WAVERIDER

作品数：15被引量：65H指数：6
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相关领域：航空宇航科学技术更多>>
相关作者：郭洪福孙拓关朝斌叶伟强傅孙成更多>>
相关机构：香港理工学院中国科学院北京理工大学更多>>
相关期刊：《International Journal of Plant Engineering and Management》《Advances in Aerodynamics》《航空动力学报》《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》更多>>
相关基金：国家自然科学基金国家教育部博士点基金更多>>
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Variable leading-edge cone method for waverider design
《Chinese Journal of Aeronautics》2025年第3期262-279,共18页Zhihao LI Chongwen JIANG Shuyao HU Chun-Hian LEE 
supported by grants from the National Natural Science Foundation of China(No.U20B2006);the Guangdong Basic and Applied Basic Research Foundation(No.2022A1515110145);Young Elite Scientists Sponsorship Program by China Association for Science and Technology(No.2022QNRC001).
The optimization of the waverider is constrained by the reversely designed leading edge and the constant shock angle distribution. This paper proposes a design method called the variable Leading-Edge Cone (vLEC) metho...
关键词：Hypersonic vehicles Waverider design methods Leading-edge cone method Variable shock angles Direct design method 
Recent development of integrated design and improving methods of waverider and inlet
《Advances in Aerodynamics》2024年第1期81-104,共24页Tianyu Gong Yaosong Long Zhongtao Cheng Yiqing Li 
This study was supported in part by the National Natural Science Foundation of China(No.61903146).
For its outstanding aerodynamic capabilities,the integrated design of the waverider and inlet is widely accepted in hypersonic aircraft.Three aspects of the integrated design of the waverider and inlet since 2020 are ...
关键词：WAVERIDER Three-dimensional inward turning inlet Integrated design Improving method 
Design methodology of an osculating cone waverider with adjustable sweep and dihedral angles被引量：1
《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》2020年第9期770-782,共13页Shao-hua CHEN Jun LIU Wei HUANG Feng DING 
Project supported by the National Natural Science Foundation of China(No.11702322);the Natural Science Foundation of Hunan Province,China(No.2018JJ3589)。
When considering the practical engineering application of a waverider,the on-design and off-design aerodynamic characteristics of the design conditions,especially the lift-to-drag ratio and the stability,deserve atten...
关键词：Osculating cone waverider Planform leading-edge profile curve Sweep and dihedral angles Lift-to-drag ratio Lateral static stability 
Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface被引量：7
《Science China(Physics,Mechanics & Astronomy)》2020年第5期124-126,共3页GuangLi Li Kai Cui YingZhou Xu HaoXiang Wang Jing Yang XianGui Xu 
supported by the National Natural Science Foundation of China(Grant No.11572333);the State Key Laboratory of High Temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences(Grant No.LHD2017TC01);the Chinese Academy of Sciences Foundation Frontier Scientific Research Program(Grant No.ZDBS-LY-JSC005)。
Lift-to-drag ratio (L/D) is nearly the most important index in determining the aerodynamic performance of a hypersonic flight vehicle,because the flight distance is linearly proportional to the L/D according to Bregue...
关键词：CONFIGURATION SHAPED PURSUIT 
Performance comparison between waverider and wide-speed-range gliding vehicle based on CFD approaches被引量：1
《Science China(Technological Sciences)》2019年第10期1861-1870,共10页ZHANG TianTian WANG ZhenGuo HUANG Wei YAN XiaoTing 
supported by the National Natural Science Foundation of China(Grant No.11502291)
Wide-speed-range gliding vehicle(WSRGV) is designed to adapt to the variable cruising environment that hypersonic vehicles will encounter during the mission implementation. Based on the cone-derived theory, a novel de...
关键词：wide-speed RANGE cone-derived WAVERIDER VOLUMETRIC efficiency lift-to-drag ratio loading property 
Design and experimental study of a practical Osculating Inward Cone Waverider Inlet被引量：9
《Chinese Journal of Aeronautics》2016年第6期1582-1590,共9页He Xuzhao Zhou Zheng Qin Si Wei Feng Le Jialing 
supported by the National Natural Science Foundation of China (Nos. 51376192 and 91216303)
A design method based on tip to tail streamline tracing and osculating inward cone methods is discussed for designing the integrated Osculating Inward Cone Waverider Inlet（OICWI）. A practical geometrical constrained...
关键词：INLET Integration design Inward turning cone WAVERIDER Wind tunnel experiment 
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets被引量：10
《Science China(Technological Sciences)》2013年第8期1980-1988,共9页CUI Kai HU ShouChao LI GuangLi QU ZhiPeng SITU Ming 
supported by the National Natural Science Foundation of China (Grant No. 90916013);the guidance and help from Academician Li Tian and peer reviewers are gratefully acknowledged
To aim at design requirements of high lift-to-drag ratio as well as high volumetric efficiency of next generation hypersonic airplanes,a body-wing-blending configuration with double flanking air inlets layout is prese...
关键词：HYPERSONIC flanking air inlet WAVERIDER computational fluid dynamics（CFD） 
A parameterized geometry design method for inward turning inlet compatible waverider被引量：5
《Chinese Journal of Aeronautics》2013年第5期1135-1146,共12页Tian Chao Li Ni Gong Guanghong Su Zeya 
supported by the National Natural Science Foundation of China (Grant No.61004089)
Intensive studies have been carried out on generations of waverider geometry and hypersonic inlet geometry. However, integration efforts of waverider and related air-intake system are restricted majorly around the X43...
关键词：Hypersonic inlets Hypersonic vehicles Inward turning inlet Optimization PARAMETERIZATION WAVERIDER 
6种典型飞行器的RANS计算及大分离区域的DES分析被引量：1
《航空动力学报》2012年第3期481-495,共15页王保国 郭洪福 孙拓 安二 关朝斌 
国家自然科学基金(50376004);高等学校博士学科点专项基金(20030007028)
提出了一种将RANS(Reynolds averaged Navier-Stokes)与DES(detached eddy simulation)相结合计算流场的工程新算法,并用于第一代载人飞船Mercury、第二代载人飞船Gemini、人类第一枚成功到达火星上空的Fire-Ⅱ探测器、具有丰富风洞实...
关键词：RANS(Reynolds averaged Navier-Stokes) DES(detached EDDY simulation) Mercury飞船 Gemini飞船 Fire-Ⅱ火星探测器 WAVERIDER CAV(common aero vehicle) 
Aerodynamic characteristics research on wide-speed range waverider configuration被引量：9
《Science China(Technological Sciences)》2009年第10期2903-2910,共8页WANG FaMin DING HaiHe LEI MaiFang 
Supported by the National Natural Science Foundation of China (Grant No. 10772186);the Key Foundation of National Natural Science Foundation of China (Grant No. 90505016)
Waverider generated from a given flow field has a high lift-to-drag ratio because of attached bow shock on leading edge. However, leading edge blunt and off-design condition can make bow shock off leading edge and hav...
关键词：WAVERIDER CONFIGURATION aerodynamic characteristics at wide-speed RANGE high lift-to-drag ratio 
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