检索结果-南通市图书馆

Chinese Journal of Aeronautics 2007年第4期20卷 289-296页

作者： han zhonghua he fei song wenping qiao zhide National Key Laboratory of Aerodynamic Design and Research School of Aeronautics Northwestern Polytechnical University Xi ＇an 710072 China

To develop an efficient and robust aerodynamic analysis method for numerical optimization designs of wing and complex configuration, a combination of matrix preconditioning and multigrid method is presented and investigated. The time derivatives of three-dimensional Navier-Stokes equations are preconditioned by Choi-Merkle preconditioning matrix that is originally designed for two-dimensional low Mach number viscous flows. An extension to three-dimensional viscous flow is implemented, and a method improving the convergence for transonic flow is proposed. The space discretizaition is performed by employing a finite-volume cell-centered scheme and using a central difference. The time marching is based on an explicit Rtmge-Kutta scheme proposed by Jameson. An efficient FAS multigrid method is used to accelerate the convergence to steady-state solutions. Viscous flows over ONERA M6 wing and M100 wing are numerically simulated with Mach numbers ranging from 0.010 to 0.839. The inviscid flow over the DLR-F4 wing-body configuration is also calculated to preliminarily examine the performance of the presented method for complex configuration. The computed results are compared with the experimental data and good agreement is achieved. It is shown that the presented method is efficient and robust for both compressible and incompressible flows and is very attractive for aerodynamic optimization designs of wing and complex configuration.

关键词： Navier-Stokes equations preconditioning method multigrid method numerical simulation

在线全文

学校读者我要写书评

暂无评论

零质量射流推迟翼型失速的数值模拟

航空学报 2007年第5期28卷 1040-1046页

作者：韩忠华乔志德宋文萍西北工业大学航空学院翼型叶栅空气动力学国防科技重点实验室陕西西安710072

通过在具有分离流动的翼型表面局部地引入零质量射流干扰,可以较小的能量代价实现对翼型绕流的全局性主动控制,从而达到抑制分离、推迟翼型失速的目的。本文发展了零质量射流与翼型绕流干扰的数值分析方法。在格心有限体积法的基础上,... 详细信息

通过在具有分离流动的翼型表面局部地引入零质量射流干扰,可以较小的能量代价实现对翼型绕流的全局性主动控制,从而达到抑制分离、推迟翼型失速的目的。本文发展了零质量射流与翼型绕流干扰的数值分析方法。在格心有限体积法的基础上,空间离散采用AUSM+-up格式,时间推进运用含牛顿型LU-SGS子迭代的全隐式双时间法,且引入了预处理方法和多重网格法等技术。以TAU0015翼型失速主动控制为算例,通过在翼型上表面前缘附近引入零质量射流控制,使翼型失速特性得到改善。将计算结果与实验结果做了比较,验证了本文发展的数值模拟方法及程序的正确性。还以NACA0015翼型为例研究了射流动量系数、射流频率、射流偏角等关键参数对失速控制效果的影响,得出一些关于如何选择控制参数的结论。

关键词：主动流动控制零质量射流 N-S方程预处理方法多重网格法

一种隐式预处理方法及其在定常和非定常流动数值模拟中的应用

在线全文

学校读者我要写书评

暂无评论

计算物理 2009年第5期26卷 679-684页

作者：韩忠华宋文萍乔志德翼型、叶栅空气动力学国防科技重点实验室西北工业大学航空学院陕西西安710072

将Choi-Merkle矩阵预处理方法与LU-SGS隐式方法、双时间法以及多重网格方法结合,发展适用于绕飞行器定常和非定常粘性流动的高效隐式预处理计算方法和程序.介绍一种针对定常和非定常流动的LU-SGS隐式预处理方法的统一表述方法.在不改变... 详细信息

将Choi-Merkle矩阵预处理方法与LU-SGS隐式方法、双时间法以及多重网格方法结合,发展适用于绕飞行器定常和非定常粘性流动的高效隐式预处理计算方法和程序.介绍一种针对定常和非定常流动的LU-SGS隐式预处理方法的统一表述方法.在不改变流动解的前提下,对Navier-Stokes方程的伪时间导数项实施Choi-Merkle矩阵预处理,从而改善可压缩控制方程在低速情况下的系统刚性,使基于LU-SGS时间推进格式的数值模拟方法同时适用于从极低马赫数到可压缩范围内的数值模拟.对Jameson中心格式的人工粘性进行相应的修改,以提高低速流动的计算精度.翼型、机翼以及翼身组合体绕流的数值模拟研究表明,隐式预处理方法获得了很高的计算效率,可使马赫数0.1左右的低速流动计算时间减少50%以上;通过对现有可压缩计算程序进行小量改动,便可使其均匀覆盖整个低速流动范围,提高CFD程序在飞行器绕流数值模拟中的实用性.

关键词： Navier-Stokes方程预处理方法 LU-SGS格式多重网格方法数值模拟

YLSG107高升力翼型主动流动控制的数值模拟

在线全文

学校读者我要写书评

暂无评论

计算物理 2009年第6期26卷 837-841页

作者：韩忠华宋文萍乔志德翼型、叶栅空气动力学国防科技重点实验室西北工业大学航空学院陕西西安710072

数值模拟零质量射流与YLSG 107翼型绕流的干扰流场,探讨零质量射流在高升力翼型失速控制中的控制效果、控制特性及控制机理.数值模拟以积分形式雷诺平均Navier-Stokes(N-S)方程为控制方程,采用格心有限体积法进行求解.通过在喷口上施加... 详细信息

数值模拟零质量射流与YLSG 107翼型绕流的干扰流场,探讨零质量射流在高升力翼型失速控制中的控制效果、控制特性及控制机理.数值模拟以积分形式雷诺平均Navier-Stokes(N-S)方程为控制方程,采用格心有限体积法进行求解.通过在喷口上施加非定常边界吹/吸边界条件模拟射流对翼型绕流的干扰.采用与风洞实验相同的来流状态和控制参数进行数值模拟,得到与实验相吻合的结果.为进一步研究控制特性和控制规律、提出改进的实验方案,研究不同动量系数、不同射流偏角对控制效果的影响,并对法向射流和近切向射流进行较深入的比较.研究表明,先前的风洞实验对应的射流动量系数(0.000 014)偏小是控制效果不显著的重要原因之一,必须达到0.001以上才有明显控制效果(射流动量系数为0.005时可使该翼型失速迎角增大2°,最大升力提高8.7%);近切向射流在失速控制方面明显优于法向射流.

关键词：主动流动控制零质量射流失速 Navier-Stokes方程高升力翼型

基于代理模型的高效全局气动优化设计方法研究进展

在线全文

学校读者我要写书评

暂无评论

航空学报 2020年第5期41卷 25-65页

作者：韩忠华许晨舟乔建领柳斐池江波孟冠宇张科施宋文萍西北工业大学航空学院气动与多学科优化设计研究所翼型、叶栅空气动力学重点实验室西安710072

基于高可信度计算流体力学的数值优化设计方法,在提高飞行器气动与综合性能方面正发挥着越来越重要的作用。基于代理模型的优化算法(SBO),由于能够实现高效全局优化,逐渐成为了气动优化设计领域的研究热点之一。近20年来,代理优化算法... 详细信息

基于高可信度计算流体力学的数值优化设计方法,在提高飞行器气动与综合性能方面正发挥着越来越重要的作用。基于代理模型的优化算法(SBO),由于能够实现高效全局优化,逐渐成为了气动优化设计领域的研究热点之一。近20年来,代理优化算法研究已取得了长足进步,多种先进的新型代理模型被提出,优化理论和算法也不断完善和发展。以飞行器精细化气动优化设计为背景,综述了基于代理模型的高效全局气动优化设计方法研究进展。首先,介绍了基于变可信度代理模型的气动优化设计方法、结合代理模型和伴随方法的气动优化设计方法以及基于非生物进化的并行气动优化设计方法的研究现状和最新进展。然后,针对飞行器气动优化设计学科领域的前沿问题,介绍了基于代理模型的多目标气动优化设计方法、混合反设计/优化设计方法、稳健气动优化设计方法的研究进展,以及基于代理模型的多学科优化设计方法的研究进展。文献综述表明,代理优化算法在设计效率、全局性以及鲁棒性等方面性能优良,已经发展到可以解决100维(100个设计变量)以内的气动优化设计问题,具有良好的工程应用前景。最后,探讨了基于代理模型的高效全局气动优化设计在理论、方法及飞行器设计应用方面所面临的问题和挑战,给出了未来研究方向的建议。

关键词：气动优化设计多学科优化设计代理模型代理优化计算流体力学

CEPC Technical Design Report

在线全文

学校读者我要写书评

暂无评论

Radiation Detection Technology and Methods 2024年第1期8卷 I0003-I0016,1-1091页

作者： Waleed Abdallah Tiago Carlos Adorno de Freitas Konstantin Afanaciev Shakeel Ahmad Ijaz Ahmed Xiaocong Ai Abid Aleem Wolfgang Altmannshofer Fabio Alves Weiming An Rui An Daniele Paolo Anderle Stefan Antusch Yasuo Arai Andrej Arbuzov Abdesslam Arhrib Mustafa Ashry Sha Bai Yu Bai Yang Bai Vipul Bairathi Csaba Balazs Philip Bambade Yong Ban Tripamo Bandyopadhyay Shou-Shan Bao Desmond P.Barber Ayse Bat Varvara Batozskaya Subash Chandra Behera Alexander Belyaev Michele Bertucci Xiao-Jun Bi Yuanjie Bi Tianjian Bian Fabrizio Bianchi Thomas Biekotter Michela Biglietti Shalva Bilanishvili Deng Binglin Denis Bodrov Anton Bogomyagkov Serge Bondarenko Stewart Boogert Maarten Boonekamp Marcello Borri Angelo Bosotti Vincent Boudry Mohammed Boukidi Igor Boyko Ivanka Bozovic Giuseppe Bozzi Jean-Claude Brient Anastasiia Budzinskaya Masroor Bukhari Vladimir Bytev Giacomo Cacciapaglia Hua Cai Wenyong Cai Wujun Cai Yijian Cai Yizhou Cai Yuchen Cai Haiying Cai Huacheng Cai Lorenzo Calibbi Junsong Cang Guofu Cao Jianshe Cao Antoine Chance Xuejun Chang Yue Chang Zhe Chang Xinyuan Chang Wei Chao Auttakit Chatrabhuti Yimin Che Yuzhi Che Bin Chen Danping Chen Fuqing Chen Fusan Chen Gang Chen Guoming Chen Hua-Xing Chen Huirun Chen Jinhui Chen Ji-Yuan Chen Kai Chen Mali Chen Mingjun Chen Mingshui Chen Ning Chen Shanhong Chen Shanzhen Chen Shao-Long Chen Shaomin Chen Shiqiang Chen Tianlu Chen Wei Chen Xiang Chen Xiaoyu Chen Xin Chen Xun Chen Xurong Chen Ye Chen Ying Chen Yukai Chen Zelin Chen Zilin Chen Gang Chen Boping Chen Chunhui Chen Hok Chuen Cheng Huajie Cheng Shan Cheng Tongguang Cheng Yunlong Chi Pietro Chimenti Wen han Chiu Guk Cho Ming-Chung Chu Xiaotong Chu Ziliang Chu Guglielmo Coloretti Andreas Crivellin hanhua Cui Xiaohao Cui Zhaoyuan Cui Brunella D'Anzi Ling-Yun Dai Xinchen Dai Xuwen Dai Antonio De Maria Nicola De Filippis Christophe De La Taille Francesca De Mori Chiara De Sio Elisa Del Core Shuangxue Deng Wei-Tian Deng Zhi Deng Ziyan Deng Bhupal Dev Tang Dewen Biagio Di Micco Ran Ding Siqin Dingl Yadong Ding Haiyi Dong Jianin AGH University of Science and Technology Faculty of Physics and Applied Computer ScienceKrakow Anhui University HefeiAnhui Applied Physics Department Federal Urdu University of ArtsScience and TechnologyIslamabad Banaras Hindu University Institute of ScienceVaranasi Bandirma Onyedi Eylul University Bandirma Beihang University Beijing Beijing Computational Science Research Center Beijing Beijing Conveyi LTD Beijing Beijing Glass Research Institute Co. LtdBeijing Beijing Institute of Technology Beijing Beijing Normal University Beijing Brown University ProvidenceRI Budker Institute of Nuclear Physics Novosibirsk Cadi Ayyad University Laboratory of Fundamental and Applied PhysicsPolydisciplinary FacultyMarrakech Cairo University Giza Center for Theory and Computation National Tsing Hua UniversityHsinchu Central China Normal University WuhanHubei Central South University ChangshaHunan Centro de Fisica Teorica de Particulas Universidade Tecnica de LisboaLisboa Chengdu KaitengSifang Digital Radio&TV Equipment Co. LtdChengduSichuan China academy of engineering physics MianyangSichuan China building materials academy Beijing China Center of Advanced Science and Technology Beijing China Institute of Atomic Energy Beijing China Jiliang University HangzhouZhejiang China Nuclear Instrument CO. LTDBeijing China University of Geosciences Beijing China University of Geosciences WuhanHubei China University of Mining and Technology XuzhouJiangsu China West Normal University NanchongSichuan Chongqing University Department of PhysicsChongqing Chulalongkorn University Bangkok City University of Hong Kong Department of PhysicsHong Kong Cockcroft Institute Daresbury Cornell University IthacaNY CPPM(AMU/IPhU&CNRS/INP) Marseille Dalian Minzu University DalianLiaoning Dalian University of Technology Department of PhysicsDalian Deutsches Elektronen-Synchrotron DESY Hamburg Dzhelepov Laboratory of Nuclear Problems of Joint Institute for Nuclear Research(DLNP JINR) Dubna East China University Of Science And Technol

The Circular Electron Positron Collider(CEPC)is a large scientific project initiated and hosted by China,fostered through extensive collaboration with international *** complex comprises four accelerators:a 30 GeV Linac,a 1.1 GeV Damping Ring,a Booster capable of achieving energies up to 180 GeV,and a Collider operating at varying energy modes(Z,W,H,and tt).The Linac and Damping Ring are situated on the surface,while the subterranean Booster and Collider are housed in a 100 km circumference underground tunnel,strategically accommodating future expansion with provisions for a potential Super Proton Proton Collider(SPPC).The CEPC primarily serves as a Higgs *** its baseline design with synchrotron radiation(SR)power of 30 MW per beam,it can achieve a luminosity of 5×10^(34)cm^(-2)s^(-1)per interaction point(IP),resulting in an integrated luminosity of 13 ab^(-1)for two IPs over a decade,producing 2.6 million Higgs *** the SR power to 50 MW per beam expands the CEPC's capability to generate 4.3 million Higgs bosons,facilitating precise measurements of Higgs coupling at sub-percent levels,exceeding the precision expected from the HL-LHC by an order of *** Technical Design Report(TDR)follows the Preliminary Conceptual Design Report(Pre-CDR,2015)and the Conceptual Design Report(CDR,2018),comprehensively detailing the machine's layout,performance metrics,physical design and analysis,technical systems design,R&D and prototyping efforts,and associated civil engineering ***,it includes a cost estimate and a preliminary construction timeline,establishing a framework for forthcoming engineering design phase and site selection *** is anticipated to begin around 2027-2028,pending government approval,with an estimated duration of 8 *** commencement of experiments and data collection could potentially be initiated in the mid-2030s.

关键词： initiated exceeding precise