Paper Title:
SPH Method Based on Bird Impact Numerical Simulation of Aircraft Engine Fan
  Abstract

The traditional numerical methods about calculation of bird strike problems are Lagrangian numerical method and Euler method. However, the existence of the finite element mesh distortion and the problem of insufficient accuracy appeared respectively. In this paper, the SPH meshless method applied to simulate bird strike aircraft engine fan, by comparing the simulated data and experimental data to test the accuracy of the simulation about bird hit the fan that is used SPH method .And by comparing the SPH method and traditional methods of bird strike problems in the time step to prove the superiority of the SPH method.

  Info
Periodical
Advanced Materials Research (Volumes 328-330)
Chapter
Chapter 1: Manufacturing Technology and Processing
Edited by
Liangchi Zhang, Chunliang Zhang and Zichen Chen
Pages
441-445
DOI
10.4028/www.scientific.net/AMR.328-330.441
Citation
B. D. Hou, Y. Xu, J. H. Yang, L. C. Peng, "SPH Method Based on Bird Impact Numerical Simulation of Aircraft Engine Fan", Advanced Materials Research, Vols. 328-330, pp. 441-445, 2011
Online since
September 2011
Export
Price
$32.00
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