Effective method for an objective estimation of small effects in air turbine engines

Authors

  • Bulat Rinatovich Abdullin
  • Vladimir Petrovich Alatorcev
  • Andrey Aleksandrovich Volik
  • Haydar Sagitovich Gumerov

Keywords:

Авиационный газотурбинный двигатель; математическое моделирование; реактивное сопло; проточная часть; утечка

Abstract

The method of the solution of a problem is considered according to influence of small design changes in a flowing part two spool mixed flow turbofan, connected with replacement of a jet nozzle of the axisymmetrical jet nozzle with controlled thrust vector.

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Published

2018-18-09

Issue

Vol. 11 No. 2 (29) (2008): Вестник УГАТУ

Section

MECHANICAL ENGINEERING AND ENGINEERING SCIENCE