云南高校图书馆联盟文献共享服务平台- SUPERSONIC

SUPERSONIC: 作品数：366被引量：791H指数：14; 导出分析报告; 相关领域：理学更多>>; 相关作者：陈怀海王亮贺旭东唐登斌朱孙科更多>>; 相关机构：南京航空航天大学上海理工大学南京理工大学哈尔滨医科大学附属肿瘤医院更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金国家重点基础研究发展计划中国博士后科学基金国家教育部博士点基金更多>>

Numerical simulation of 3D supersonic asymmetric truncated nozzle based on k-kL algebraic stress model: 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》2025年第3期238-251,共14页Gang WANG Shuai ZHANG Jifa ZHANG Yao ZHENG; supported by the Zhejiang Provincial Key Research and Development Program of China(No.2020C01020).; The nozzle is a critical component responsible for generating most of the net thrust in a scramjet engine.The quality of its design directly affects the performance of the entire propulsion system.However,most turbule...; 关键词：Supersonic nozzle Turbulence model Numerical simulation Performance analysis

Space-marching inverse design of subsonic,transonic,and supersonic internal flowfields: 《Chinese Journal of Aeronautics》2025年第2期15-30,共16页Bo ZHANG Shihe YI Yuxin ZHAO Rui YANG Ziyuan ZHU Ruitong ZENG; supported by the National Key Research and Development Program of China(No.2019YFA0405300);the National Natural Science Foundation of China(No.12272405).; Flowfield inverse design can obtain the desired flow and contour with high design efficiency,short design cycle,and small modification need.In this study,the Euler equations are formulated in the stream-function coord...; 关键词：Flowfield Inverse design Compressible flow CONTRACTION Nozzle Asymmetric channel

Aerodynamic Design Method and Experimental Investigation of a High-Load Supersonic Compressor Cascade: 《Journal of Thermal Science》2024年第6期2075-2088,共14页YAN Tingsong YAN Peigang LIANG Zhuoming CHEN Huanlong; funded by the National Science and Technology Major Project(J2019-II-0016-0037).; The high-load compressor plays an important role in further improving the performance of aero-engine.However,the complex shock waves in the cascade channel also bring more aerodynamic losses.This paper proposes a supe...; 关键词：unique inlet flow angle supersonic cascade aerodynamic optimization shock reflection pl cascadeexperiment

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

Attenuation of boundary-layer instabilities for natural laminar flow design on supersonic highly swept wings: 《Chinese Journal of Aeronautics》2024年第11期118-137,共20页Han NIE Wenping SONG Zhonghua HAN Kefeng ZHENG; supported by the National Natural Science Foundation of China(No.12072285);the National Key Research and Development Program of China(No.2023YFB3002800);the Youth Innovation Team of Shaanxi Universities,China。; To meet the challenge of drag reduction for next-generation supersonic transport aircraft,increasing attention has been focused on Natural Laminar Flow(NLF)technology.However,the highly swept wings and high-Reynolds-n...; 关键词：Supersonic transport aircraft Natural laminar flow design Supersonic flow Highly-swept wings Transition delay Linear stability theory

Preferential concentration in supersonic gas-particle two-phase transverse jets: 《Particuology》2024年第11期29-47,共19页Likun Ma Luxi Xu Kangchun Zhao Pengnian Yang Yunchao Feng Binbin Chen Zhixun Xia; supported by the National Natural Science Foundation of China(grant Nos.12272409,T2221002);Changsha Science and Technology Project(grant No.kq2107001);the Science and Technology Innovation Program of Hunan Province(grant No.2022RC1233);Hunan Provincial Innovation Foundation for Postgraduate(grant No.QL20230015).; The supersonic gas-particle two-phase transverse jet is a typical flow process in many applications,such as solid rocket scramjet.This study carried out experimental tests as well as Large Eddy Simulation(LES)to inves...; 关键词：SUPERSONIC CROSSFLOW Gas-particleflow Preferential concentration

Nonlinear metamaterial enabled aeroelastic vibration reduction of a supersonic cantilever wing plate: 《Applied Mathematics and Mechanics(English Edition)》2024年第10期1749-1772,共24页Peng SHENG Xin FANG Dianlong YU Jihong WEN; supported by the National Natural Science Foundation of China(Nos.52241103,52322505,and 11991032);the Natural Science Foundation of Hunan Province of China(No.2023JJ10055)。; The violent vibration of supersonic wings threatens aircraft safety.This paper proposes the strongly nonlinear acoustic metamaterial(NAM)method to mitigate aeroelastic vibration in supersonic wing plates.We employ the...; 关键词：nonlinear acoustic metamaterial(NAM) hypersonic aeroelastic vibration vibration reduction fluid-structure interaction

Effect of Sweptback Angle of a Delta Wing on Surface Pressure Distribution at Supersonic Mach Numbers: 《Fluid Dynamics & Materials Processing》2024年第10期2353-2376,共24页Shamitha Shetty Asha Crasta Sher Afghan Khan Abdul Aabid Muneer Baig; The purpose of this work is to shed light on the effect of the pivot position on the surface pressure distribution over a 3D wing in different flight conditions.The study is intended to support the design and developm...; 关键词：Mach number angles of incidence stability analysis performance optimization

Control of Nozzle Flow Using Rectangular Ribs at Sonic and Supersonic Mach Numbers: 《Fluid Dynamics & Materials Processing》2024年第8期1847-1866,共20页Vigneshvaran Sethuraman Parvathy Rajendran Sher Afghan Khan Abdul Aabid Muneer Baig; This study deals with base pressure management in a duct for various values of the Mach number(M),namely,Mach number corresponding to sonic and four supersonic conditions.In addition to the Mach number,the nozzle pres...; 关键词：Base pressure internal flows RIBS suddenly expanded flow wall pressure

Large eddy simulation of boundary layer combustion of hydrogen and hydrocarbon fuel films in a modeled scramjet combustor: 《Chinese Journal of Aeronautics》2024年第7期109-133,共25页Jianfei WEI Silong ZHANG Jingying ZUO Xin LI Jiang QIN Wen BAO; supported by the National Natural Science Foundation of China(No.52176037).; Supersonic fuel film cooling is a promising way to simultaneously reduce the severe wall heat and friction load of the internal passage in a scramjet engine when operating at hypersonic conditions.Large eddy simulatio...; 关键词：Supersonic film cooling HYDROGEN HYDROCARBON Boundary layer combustion Large eddy simulation

SUPERSONIC