Development of the universal software complex for solving optimization problems of parameters and flow path of GTE using models with private code

Authors

  • Igor Aleksandrovich Krivosheev
  • Yuliya Andreevna Hohlova
  • Roman Alekseevich Zavyalov

Keywords:

aircraft engines; optimization; turbine GTE; GTE parameter optimization.

Abstract

Consider the problems of multivariate optimization in the design of aircraft engines and their components. The necessity of using in this case software systems designed in different bureaus shown. Presented results of the creation and use in solving problems by the universal software system optimizer developed by the authors.

Published

2018-07-08

Issue

Section

AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY