VESTNIK of Samara University. Aerospace and Mechanical EngineeringVESTNIK of Samara University. Aerospace and Mechanical Engineering2542-04532541-7533Samara National Research University276110.18287/2541-7533-2011-0-5(29)-208-214UnknownAnalysis of combustion models applicability for designing combustion chamber with a large number of nozzlesMingazovB. G.<p>Doctor of Technical Sciences, Professor</p>
<p>Head of the Department of Aircraft Engines and Power Plants</p>ming@adeu.kstu-kai.ruYavkinV. B.<p>Candidate of Technical Sciences</p>
<p>Associate Professor of the Department of Aircraft Engines and Power Plants</p>vb.yavkin@gmail.comSabirzyanovA. N.<p>Candidate of Technical Sciences</p>
<p>Associate Professor of the Department of Special Engines</p>sabirzan@sd.kstu-kai.ruBaklanovA. V.<p>Post-graduate Student of the Department of Aircraft Engines and Power Plants</p>andreybaklanov@bk.ruKazan State Technical UniversityKazan Research National Technical University named after A.N. Tupolev - KAI191220111052082141711201517112015Copyright © 2015, VESTNIK of the Samara State Aerospace University2015<p>Applications of models for predicting the parameters of gas-turbine engine combustion chamber process arediscussed in the paper. Characteristic simulation results for different models ofcombustion are presented.</p>Combustion chambermodelingburningturbulenceКамера сгораниямоделированиегорениетурбулентность