Method of Optimization of Blade Shapes in Aerodynamic Design of the Fan Cascade

被引:1
|
作者
E. A. Batyaev
V. B. Kurzin
机构
[1] Lavrent'ev Institute of Hydrodynamics,
[2] Siberian Division,undefined
[3] Russian Academy of Sciences,undefined
关键词
Mathematical Modeling; Mechanical Engineer; Inverse Problem; Geometric Parameter; Iterative Method;
D O I
10.1023/A:1019887802793
中图分类号
学科分类号
摘要
A method is developed for calculating the geometric parameters of the cascade of an axial fan with a given performance. The method is based on minimization of a certain functional and using the solution of an inverse problem of the flow around the cascade within the framework of the hypothesis of cylindrical cross sections. The functional is minimized by an iterative method of linearization. Examples of calculations are given.
引用
收藏
页码:701 / 705
页数:4
相关论文
共 50 条
  • [1] Aerodynamic and structural multidisciplinary optimization design method of fan rotors based on blade curvature constraints
    Song, Zhaoyun
    Zheng, Xinqian
    Wang, Baotong
    Zhou, Kai
    Adjei, Richard Amankwa
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 136
  • [2] Aerodynamic optimization of industrial fan blade cascades
    Lotfi, O.
    Teixeira, J. A.
    Ivey, P. C.
    Sheard, G.
    Kinghorn, I. R.
    [J]. Proceedings of the ASME Turbo Expo 2005, Vol 6, Pts A and B, 2005, : 1059 - 1066
  • [3] Responsiveness of Grouping Optimization Design of Multi-Blade Centrifugal Fan to Aerodynamic Performance of Fan Coil Unit
    Liu, Yang
    Liu, Xiaomin
    Chen, Zonghua
    Xi, Guang
    [J]. Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2022, 56 (07): : 156 - 167
  • [4] Optimization design of axial fan blade
    Wu, Yujing
    Huang, Diangui
    [J]. JOURNAL OF THE CHINESE INSTITUTE OF ENGINEERS, 2019, 42 (06) : 473 - 478
  • [5] Aerodynamic design method of cascade profiles based on load and blade thickness distribution
    Yao, Z
    Liu, GL
    [J]. APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2003, 24 (08) : 886 - 892
  • [6] Aerodynamic design method of cascade profiles based on load and blade thickness distribution
    Yao Zheng
    Liu Gao-lian
    [J]. Applied Mathematics and Mechanics, 2003, 24 (8) : 886 - 892
  • [7] The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade
    Hergt, Alexander
    Klinner, J.
    Steinert, W.
    Grund, S.
    Beversdorff, M.
    Giebmanns, A.
    Schnell, R.
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2015, 137 (02):
  • [8] Aerodynamic Design and Multi-Objective Optimization of an Adjustable Blade Axial-Flow Fan
    Meng, Fanjie
    Zhang, Yingkun
    Xiong, Jin
    Li, Jingyin
    [J]. International Journal of Fluid Machinery and Systems, 2022, 15 (01) : 75 - 85
  • [9] THE EFFECT OF AN ERODED LEADING EDGE ON THE AERODYNAMIC PERFOMANCE OF A TRANSONIC FAN BLADE CASCADE
    Hergt, A.
    Klinner, J.
    Steinert, W.
    Grund, S.
    Beversdorff, M.
    Giebmanns, A.
    Schnell, R.
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 2A, 2014,
  • [10] Impeller Design of a Centrifugal Fan with Blade Optimization
    Lee, Yu-Tai
    Ahuja, Vineet
    Hosangadi, Ashvin
    Slipper, Michael E.
    Mulvihill, Lawrence P.
    Birkbeck, Roger
    Coleman, Roderick M.
    [J]. INTERNATIONAL JOURNAL OF ROTATING MACHINERY, 2011, 2011