Advanced Search
Volume 38 Issue 4
Apr.  2012
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (4): 563-568.
Su Yuqin, Zhang Zuoguang. Synthesis and Performance of Macroporous Anion Exchange Resin[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(6): 493-496. (in Chinese)
Citation: Yuan Wu, Yan Chao, Xi Keet al. Investigation and enhancement of hole mapping method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (4): 563-568. (in Chinese)
shu

Investigation and enhancement of hole mapping method

  • National Key Laboratory of Computational Fluid Dynamics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 24 Dec 2010
  • Publish Date: 30 Apr 2012
    Abstract
  • In order to reduce the storage of the traditional hole mapping method, a minimum hole mapping algorithm was presented which expands the concept of closure. Wall surface was allowed to terminate on truncation surface of grids, which would efficiently reduce the area of hole mapping and save the storage. Methods of hole mapping cell identification suitable for the generalized closure were analyzed, showing the unreliability of using wall surface information to identify the property of hole mapping cell. A new method named Inverse mark was developed which is especially suitable to the generalized closure. Mesh nodes- information was used to automatically identify out points, which are initial points to advance inside of the grid region. Results show that Inverse mark is of great efficiency, good reliability, and high automation, and can effectively enhance the flexibility of chimera grids to local complex configurations such as slits.

     

    • FullText(HTML)
    • References(13)
  • [1]
    Ralph W N, Jeffrey P S. A summary of the 2004 overset symposium on composite grids and solution technology. AIAA-2005-921, 2005
    [2]
    Benek J A, Buning P G, Steger J L. A 3-D Chimera grid embedding technique. AIAA-85-1523, 1985
    [3]
    Bonet J, Peraire J. An alternating digital tree (ADT) algorithm for 3D geometric searching and intersection problems[J]. International Journal for Numerical Methods in Engineering, 1991, 31(1):1-17
    [4]
    Chiu I T,Meakin R L. On automating domain connectivity for overset grids. AIAA-95-0854, 1995
    [5]
    Meakin R. Object X-ray for cutting holes in composite overset structured grids. AIAA-2001-2537, 2001
    [6]
    Sudharsun Jagannathan. A methodology for assembling overset generalized grids. Mississippi: Computational Engineering in the College of Engineering, Mississippi State University, 2004
    [7]
    Sogers S E, Suhs N E, Dietz W E. PEGSUS 5: an automated pre-processor for overset-grid computational fluid dynamics[J]. AIAA Journal, 2003, 41(6):1037-1045
    [8]
    李亭鹤.重叠网格自动生成方法研究. 北京:北京航空航天大学航空科学与工程学院,2004 Li Tinghe. Investigation of chimera grid automatic generation algorithm. Beijing: School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, 2004(in Chinese)
    [9]
    范晶晶.复杂重叠网格方法研究及多体运动的非定常流动模拟. 北京:北京航空航天大学航空科学与工程学院,2010 Fan Jingjing. Enhancement of complex overset grid assembly and numerical simulation of unsteady multi-body movement. Beijing: School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, 2010(in Chinese)
    [10]
    阎超.计算流体力学方法及应用[M]. 北京:北京航空航天大学出版社,2006:245-248 Yan Chao. The methodology and application of computational fluid dynamics[M]. Beijing: Beihang University Press, 2006:245-248(in Chinese)
    [11]
    Taylor S, Johnson C T. Launch-vehicle simulations using a concurrent, implicit Navier-Stokes solver. AIAA-95-0223, 1995
    [12]
    Spinetti R L, Jolly B A. Time-accurate numerical simulation of GBU-38s separating from the B-1B aircraft with various ejector forces, store properties, and load-out configurations. AIAA-2008-187, 2008
    [13]
    张辉,重叠网格技术在飞行器多体分离问题中的应用. 北京:北京航空航天大学航空科学与工程学院,2010 Zhang Hui. The overlapping grid technology in the application of multi-body separation problem in the aerocraft. Beijing: School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, 2010(in Chinese)
    • Relative Articles

  • Relative Articles

    [1]YANG X J，ZHANG X L，LI P R. Performance of Gyroid heat exchanger based on structural parameters analysis[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（4）：1195-1204 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0245.
    [2]JIANG Xingyu, XUE Fengfeng, JIANG Fanghua, SHI Peng, GONG Shengping. An adaptive improved PD controller for rigid-elastic coupled launch vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0383
    [3]BAI Jianfeng, MENG Junhui, ZHANG Lili, WEI Shechun, MA Nuo. Dynamic performances research of the wing deployment considering fluid structure interaction[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0645
    [4]HAN H，HAO J，ZHANG Q K，et al. Multi-source knowledge fusion model for aspect-based sentiment analysis[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（9）：2688-2695 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0728.
    [5]CAI Shu-yu, HE Chong. A damage detection method for aero-engine based on FDG-YOLO lightweight model[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0024
    [6]WANG Ming-jian, ZHAO Zhang-hai, LI Chao, WEN Jia-min, SHANG Min-qiang, HOU Hong-jun. HPC Fault and Performance Analysis in the Field of Petroleum Geophysical Exploration[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0768
    [7]XU Y，GUO H J，CHAO L D，et al. Design and analysis of ground test control circuit on liquid rocket engine[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（7）：2245-2255 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0614.
    [8]ZHANG Hua-bo, GUO Ying-qing, LI Gui-cai, ZHAO Wan-li, YE Peng. Modeling and parameter design methodology for component-level performance model of ducted ram air generation turbine[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0787
    [9]CHEN C，GE J H，XU J L，et al. Influence of inlet corner wave system on performance of scramjet nozzle[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3250-3261 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0768.
    [10]LI J，LI Q，ZUO Y J，et al. Real-time performance analysis on Terahertz interconnection with timed token protocol in avionics[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：932-942 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0317.
    [11]REN Yong-jie, XU Bo-qi, CHU Wei, GUO Kang-kang, TONG Yi-heng, NIE Wan-sheng. Effects of O/F Ratio on the Combustion Stability of a Model Rocket Engine with Hypergolic Propellant[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0444
    [12]GONG F X，LI M R. Principle and performance analysis of base station cluster location[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2567-2578 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0751.
    [13]LI Xing-fei, HAN Jia-xin, TUO Wei-xiao, LIU Ya-qi, WANG Tian-yu. Influence analysis of flexure support characteristics on performance of inertial reference unit[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0461
    [14]YANG Zhan-gang, WEI Yu-hao, SHI Xu-dong. Electrical Properties Analysis of Composite Skin Bonding Structures[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0507
    [15]WANG R C，ZHANG G X，WANG X Y，et al. Aerodynamic performance analysis of supercritical airfoil with lower surface jet[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1671-1679 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0489.
    [16]LIU Shun, KONG Xiang-rui, XU Jing-lei, GAO Bo, LIU Hai-long. Reconstruction measurement method for ramjet nozzle thrust based on PIV[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0535
    [17]GUO Qing, HUANG Qi-lian, CHEN Jin-liang. Performance Degradation Modeling of Civil Aviation Engine Based on Component Characteristic Map Optimization[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0341
    [18]GUO S N，SONG W，XIANG N L，et al. Dynamic characteristics of turbine flowmeter based on CFD simulation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1904-1911 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0594.
    [19]HE L T，FANG H R，CHEN Y F，et al. Design and performance analysis of spatial large extension parallel mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1722-1734 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0548.
    [20]YANG Zhan-gang, KE Zhong-shu, YANG Xu-wei, BAO Xing-wang. Analysis of the influence of finishing process on the electrical properties of composite skin[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2022-0763
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2241) PDF downloads(562) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return