Study of transonic drag computation on the DLR-F6 complex configurations

被引:0
|
作者
Zhang, Hong [1 ]
Yan, Hong [2 ]
机构
[1] School of Science, Chang'an University, Xi'an 710064, China
[2] Aeronautical Laboratory of Computational Fluid Dynamics, Aeronautics Computing Technique Research Institute, Xi'an, 710068, China
来源
Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University | 2013年 / 34卷 / 03期
关键词
10;
D O I
10.3969/j.issn.1006-7043.201206006
中图分类号
学科分类号
摘要
引用
收藏
页码:325 / 331
相关论文
共 49 条
  • [1] Transonic drag computation around DLR-F6 wing body configurations
    Zheng, Qiuya
    Liu, Sanyang
    Zhou, Tianxiao
    Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2010, 44 (09): : 115 - 121
  • [2] Transonic drag prediction on a DLR-F6 transport configuration
    Zheng, Qiuya
    Feng, Jianhu
    Shen, Zunhuan
    MACHINE DESIGN AND MANUFACTURING ENGINEERING, 2012, 566 : 676 - +
  • [3] Transonic drag prediction on a DLR-F6 transport configuration using unstructured grid solvers
    Lee-Rausch, E. M.
    Frink, N. T.
    Mavriplis, D. J.
    Rausch, R. D.
    Milholen, W. E.
    COMPUTERS & FLUIDS, 2009, 38 (03) : 511 - 532
  • [4] Drag of DLR-F6 wing-body configuration
    Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
    Jisuan Wuli, 2008, 2 (145-150):
  • [5] Drag Prediction on DLR-F6 Wing-Body Configuration
    Zheng, Qiuya
    Liu, Sanyang
    MECHANICAL AND AEROSPACE ENGINEERING, PTS 1-7, 2012, 110-116 : 1506 - +
  • [6] Computation of aerodynamic coefficients for the DLR-F6 configuration using MEGAFLOW
    Brodersen, O
    Monsen, E
    Ronzheimer, A
    Rudnik, R
    Rossow, CC
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS II, 1999, 72 : 85 - 92
  • [7] Drag prediction of DLR-F6 using MFlow unstructured mesh solver
    Zhang, Yao-Bing
    Deng, You-Qi
    Wu, Xiao-Jun
    Meng, Fan-Ju
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2011, 29 (02): : 163 - 169
  • [8] Drag prediction of DLR-F6 configuration with TRIP2.0 software
    Wang, Yun-Tao
    Wang, Guang-Xue
    Zhang, Yu-Lun
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2009, 27 (01): : 108 - 113
  • [9] Drag prediction for the DLR-F6 wing-body configuration using the edge solver
    Eliasson, Peter
    Peng, Shia-Hui
    JOURNAL OF AIRCRAFT, 2008, 45 (03): : 837 - 847
  • [10] DLR-F6翼身组合体阻力计算
    王运涛
    王光学
    张玉伦
    计算物理, 2008, (02) : 145 - 150