Aircraft engine design based on unified gas generator

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.

About the authors

A. S. Vinogradov

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Author for correspondence.
Email: fdla@ssau.ru

candidate of technical science
docent of department «Construction and design of aircraft engines»

Russian Federation

Ye. F. Parovay

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Email: fdla@ssau.ru

student

Russian Federation

A. G. Mordvinov

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Email: fdla@ssau.ru

student

Russian Federation

D. V. Popov

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Email: fdla@ssau.ru

student

Russian Federation

M. A. Shirokov

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Email: fdla@ssau.ru

student

Russian Federation

References

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