Study the effectiveness of the dust devices

Authors

  • Anas Saidovich Gishvarov
  • Rufat Rinatovich Aitov
  • Arman Maratovich Aytumbetov

Keywords:

mathematic modeling; helicopter gas turbine engines; dust devices; flow; two?component flow.

Abstract

 The study of the effectiveness of the dust devices  helicopter gas turbine engines. Based on the numerical  simulation of two?component flow assessed the effectiveness of various design options. 

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Published

2018-25-07

Issue

Vol. 19 No. 2 (68) (2015): Вестник УГАТУ

Section

AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY