Analysis of combustion models applicability for designing combustion chamber with a large number of nozzles

Abstract


Applications of models for predicting the parameters of gas-turbine engine combustion chamber process are discussed in the paper. Characteristic simulation results for different models ofcombustion are presented.


About the authors

B. G. Mingazov

Kazan State Technical University

Author for correspondence.
Email: ming@adeu.kstu-kai.ru

Russian Federation

Doctor of Technical Sciences, Professor

Head of the Department of Aircraft Engines and Power Plants

V. B. Yavkin

Kazan State Technical University

Email: vb.yavkin@gmail.com

Russian Federation

Candidate of Technical Sciences

Associate Professor of the Department of Aircraft Engines and Power Plants

A. N. Sabirzyanov

Kazan State Technical University

Email: sabirzan@sd.kstu-kai.ru

Russian Federation

Candidate of Technical Sciences

Associate Professor of the Department of Special Engines

A. V. Baklanov

Kazan Research National Technical University named after A.N. Tupolev - KAI

Email: andreybaklanov@bk.ru

Russian Federation

Post-graduate Student of the Department of Aircraft Engines and Power Plants

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