Published March 3, 2022
| Version v1
Conference paper
Open
Comparative analysis of design methods efficiency in Russian and foreign turbine cooling systems of multi-mode turbojet engines
Authors/Creators
- 1. Moscow Aviation Institute (National Research University), Experimental Design Office named after A. Lyulka
Description
Abstract
The researching results turbine cooling systems designs of foreign and Russian aircraft bypass turbojet engines with an afterburner are presented. For the computational research and comparative analysis, the samples of Russian and foreign advanced by-pass turbojet engines with an afterburner with the most optimal technical characteristics were selected, their cooling systems gas-dynamic parameters were calculated at 4 critical engine operating modes ...