Gas turbine engines and gas turbine power plants compressors early design stages effectiveness increase

Authors

  • Aleksandra Borisovna Mihaylova
  • Dmitriy Albertovich Ahmedzyanov
  • Aleksey Evgenevich Mihaylov

Keywords:

aircraft engines; gas turbine power plants; compressors; designing; simulation.

Abstract

The paper discusses main aspects of bundled software generation for increase of design effectiveness of gas turbine engines and gas turbine power plants compressors. The main features of the bundled software for solving direct and inverse problems in one- and twodimensional formulation, and verification results for developed gas turbine engine and gas turbine power plants compressors simulation methods are presented in the paper. The recommendations for the use of developed methods and simulation tools in the designing of gas turbine engine and gas turbine power plant compressors are given in the article.

Published

2018-07-08

Issue

Section

AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY