Paper Title:
Turbulence Model Influence on Numerical Investigation of Transonic Axial Compressor Rotor
  Abstract

Numerical method using HI and HOH meshing combined B - L turbulent model and S - A turbulent model separately based on the Rotor 37 compressor Rotor was applied to the steady flow. results on pressure characteristic curve, stall point forecast etc were compared with related experimental data. This paper discussed calculation precision influenced by the turbulence model and numerical computation grid. This numerical investigation was basis for subsequent compressor internal flow field study.

  Info
Periodical
Advanced Materials Research (Volumes 308-310)
Chapter
Structural Strength and Robustness
Edited by
Jian Gao
Pages
1519-1522
DOI
10.4028/www.scientific.net/AMR.308-310.1519
Citation
F. Xie, C. J. Liu, Y. J. Wang, "Turbulence Model Influence on Numerical Investigation of Transonic Axial Compressor Rotor", Advanced Materials Research, Vols. 308-310, pp. 1519-1522, 2011
Online since
August 2011
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Price
$32.00
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