Проектирование авиационного двигателя на основе базового газогенератора

Виноградов А. С.; A. S. Vinogradov; Паровай Е. Ф.; Ye. F. Parovay; Мордвинов А. Г.; A. G. Mordvinov; Попов Д. В.; D. V. Popov; Широков М. А.; M. A. Shirokov

doi:10.18287/2541-7533-2011-0-3-3(27)-131-139

Aircraft engine design based on unified gas generator

Authors: Vinogradov A.S.¹, Parovay Y.F.¹, Mordvinov A.G.¹, Popov D.V.¹, Shirokov M.A.¹
Affiliations:
1. Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Issue: Vol 10, No 3-3 (2011): Special Issue
Pages: 131-139
Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
URL: https://journals.ssau.ru/vestnik/article/view/6867
DOI: https://doi.org/10.18287/2541-7533-2011-0-3-3(27)-131-139
ID: 6867

Cite item

Full Text

Abstract
About the authors
References
Supplementary files
Statistics

Abstract

In article the algorithm of aircraft engine designing based on unified gas generator is considered. Also here the main stages of such model creating are described. This stages include thermogas dynamic account, blade profiling, The algorithm combines accounts of hydraulic resistance, thermal condition, unite assembling and detail data base creating, strength accounts and assemble scheme.