云南高校图书馆联盟文献共享服务平台- Advances in Aerodynamics

《Advances in Aerodynamics》: 作品数：185被引量：172H指数：6; 导出分析报告; 主办单位：中国空气动力学会; 最新期次：2024年1期更多>>; 发文主题：TURBULENCEUNIFIEDHYPERSONICAERODYNAMICSSHOCK_WAVE更多>>; 发文领域：理学航空宇航科学技术自动化与计算机技术经济管理更多>>; 发文基金：国家自然科学基金国家重点基础研究发展计划高等学校学科创新引智计划中国博士后科学基金更多>>

Study on rapid calculation and imaging simulation of aircraft infrared radiation characteristics: 《Advances in Aerodynamics》2024年第1期1-17,共17页Huicheng Yang Qingzhen Yang Yongqiang Shi Xubo Du Xinyuan Liu; This work was supported by the National Natural Science Foundation of China(12102356).; The infrared radiation characteristics of aircraft are a key focus in attack-defense confrontation and early warning detection.A rapid simulation method for calculating the infrared characteristics of targets is propo...; 关键词：Infrared radiation characteristics Infrared image simulation Rapid simulation Discrete transfer method

A novel wall interference correction method for airfoil: 《Advances in Aerodynamics》2024年第1期18-38,共21页Binbin Wei Yongwei Gao Ruiyang Qiao Shuling Hu; This work was sponsored by the National Natural Science Foundation of China(No.12302303);the China Postdoctoral Science Foundation(No.2023M732777);the foundation of National Key Laboratory of Aircraft Configuration Design(No.ZYTS-202403);the foundation of National Key Laboratory of Science and Technology on Aerodynamic Design and Research(No.2023-JCJQ-LB-070).; Corrections for wind tunnel experimental results are crucial when accounting for tun-nel wall interference.This study introduces a new method,the non-uniform wall pres-sure signature method(NUWPSM),which is designed t...; 关键词：Wind tunnel experiment Wall interference Wall interference correction AIRFOIL Non-uniform wall pressure signature method

Numerical simulation of turbulent airflow around a tall telecommunication tower model: 《Advances in Aerodynamics》2024年第1期39-80,共42页Alireza Moradi Eysa Salajegheh Mohammad Mehdi Tavakol Ali Heidari Goodarz Ahmadi; In this study,wind flow around a telecommunication tower(Milad Tower)model was numerically simulated.Several computational fluid dynamics(CFD)simulations were performed using the Reynolds Averaged Navier–Stokes(RANS)...; 关键词：Computational fluid dynamics Pressure distribution Turbulent boundary layer Milad tower Tall structure

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

Comparative study on predicting turbulent kinetic energy budget using high‑order upwind scheme and non‑dissipative central scheme: 《Advances in Aerodynamics》2024年第1期105-122,共18页Dandi Wang Yiming Du Yao Jin Jinsheng Cai Fei Liao; This work is supported by the National Natural Science Foundation of China(Nos.12102360,92152301);the Natural Science Basic Research Program of Shaanxi(Program No.2023-JC-QN-0017).; The accurate computation of different turbulent statistics poses different requirements on numerical methods.In this paper,we investigate the capabilities of two representa-tive numerical schemes in predicting mean ve...; 关键词：Non-dissipative scheme Discrete energy conservation TKE budget 30P30N airfoil

Influence of the shock wave‑turbulence interaction on the swirl distortion in hypersonic inlet: 《Advances in Aerodynamics》2024年第1期123-143,共21页Zhenlong Wu Yiqing Li Limei Lu Xinyi Xu Ranhui Liang; This research was funded by the National Natural Science Foundation of China(Grant No.12002144);the Jiangxi Provincial Natural Science Foundation(Grant No.20212BAB211015).; This study uses the Large Eddy Simulation(LES)technique to conduct an exhaustive analysis of the flow characteristics within the Rectangular-to-Elliptical shape Transition(REST)inlet under Mach 6 conditions.It mainly ...; 关键词：REST inlet Hypersonic inlet Large eddy simulation TURBULENCE Swirl distortion measurement

Multiscale simulation of rarefied gas dynamics via direct intermittent GSIS‑DSMC coupling: 《Advances in Aerodynamics》2024年第1期144-159,共16页Liyan Luo Lei Wu; This work is supported by the National Natural Science Foundation of China(No.12172162);the Stable Support Plan(No.80000900019910072348).; The general synthetic iterative scheme(GSIS)has proven its efficacy in modeling rare-fied gas dynamics,where the steady-state solutions are obtained after dozens of itera-tions of the Boltzmann equation,with minimal n...; 关键词：Direct simulation Monte Carlo General synthetic iterative scheme Fast convergence Asymptotic-preserving

On the effects of non‑zero yaw on leading‑edge tubercled wings: 《Advances in Aerodynamics》2024年第1期160-178,共19页T.H.New S.Mandra; the support for the research project by ETH Zurich;Nanyang Technological University, Singapore。; Steady-state numerical simulations were conducted to capture the aerodynamic characteristics and flow patterns resulting from a tubercled and non-tubercled wing subjected to various combined pitch and yaw conditions a...; 关键词：Leading-edge tubercles Finite wings Vortex systems Yaw Numerical simulation

Wind‑resistant design theory and safety guarantee for large oil and gas storage tanks in coastal areas被引量：1: 《Advances in Aerodynamics》2024年第1期179-209,共31页Bin Huang Xijie Liu Zhengnong Li Dabo Xin Jinke Liu Shujie Qin Tianyin Xiao Jinshuang Dong; This research was supported by the National Natural Science Foundation of China(52068019);the Hainan Provincial Natural Science Foundation of China(522RC605,520QN231 and 521RC502).; Large oil and gas storage tanks serve as crucial industrial energy infrastructures,which are usually thin-walled steel structures with large volumes and light weights,and they are sensitive to wind loads.Under the inf...; 关键词：Coastal area Large oil and gas storage tank Wind load Wind-induced response Structural dynamic characteristics Wind-induced vibration control

Open‑jet facility for bio‑inspired micro‑air‑vehicle flight experiment at low speed and high turbulence intensity: 《Advances in Aerodynamics》2024年第1期210-228,共19页Zhifeng Liu Yue Yang; This work has been supported in part by the National Natural Science Foundation of China(Grant Nos.11925201 and 11988102);the National Key R&D Program of China(Grant No.2020YFE0204200);the Xplorer Prize.; Bio-inspired micro-air-vehicles(MAVs)usually operate in the atmospheric boundary layer at a low Reynolds number and complex wind conditions including large-scale turbulence,strong shear,and gusts.We develop an open je...; 关键词：Open-jet facility Active grid MAV flight High turbulence intensity

《Advances in Aerodynamics》