The article presents assumptions of the one-dimensional model of the ASz-62IR aircraft engine. This model was developed in the AVL BOOST software. The ASz-62IR is a nine cylinder, aircraft engine in a radial configuration. It is produced by the Polish company WSK “PZL-Kalisz” S. A. The model is used for calculating parameters of the fuel stream and the air stream in intake system of the engine, as well as for the analyses of the combustion process and the exhaust flow to the external environment. The model is based on the equations describing the isentropic flow. The geometry of the channels and all parts of the model has been mapped on the basis of empirical measurements of the engine elements. The model assumes indirect injection where the gasoline was used as a fuel with the calorific value of 43.5 MJ/kg. The model assumes a mixture of a stoichiometric ratio of 14.5. This model is only part of the overall the ASz-62IR engine model. After the simulation tests on the full model the obtained results confirmed the correctness of the model used to create the mixture. It was found that the AVL BOOST software is good for the implementation of this type of work.
If the inline PDF is not rendering correctly, you can download the PDF file here.
 Wendeker M. Gęca M. Szlachetka M. Grabowski Ł. Sochaczewski R. and Barański G. 2011 “Modelling an aircraft fuel system” Combustion Engines PTNSS–2011–SC–033.
 López E. J. and Nigro N. M. 2000 “Validation of a 0D/1D Computational Code for The Design of Several Kind of Internal Combustion Engines” Technical report Centro Internacional de Métodos Computacionales en Ingeniería Instituto de Desarrollo Tecnológico para la Industria Química.
 Alqahtani A. Shokrollahihassanbarough F. and Wyszynski M. L. 2015 “Thermodynamic Simulation Comparison of AVL BOOST and Ricardo WAVE for HCCI and SI Engines Optimisation” Combustion Engines 161(2): pp. 68-72.
 Barros J. E. M. 2003 “Estudo de Motores de Combustão Interna Aplicando Análise Orientada a Objetos” Master’s thesis Universidade Federal de Minas Gerais.
 Coble A. R. Smallbone A. Bhave A. Mosbach S. Kraft M. Niven P. and Amphlet S. 2011 “Implementing Detailed Chemistry and In-Cylinder Stratification Into 0/1-D IC Engine Cycle Simulation Tools” SAE Technical Paper 2011-01-0849.
 Guzzella L. and Onder CH. 2010. “Introduction to modelling and control of internal combustion engine systems” Springer Berlin.
 Baumgarten C. 2010 “Mixture Formation in Internal Combustion Engine” Springer-Verlag Berlin Heidelberg Stiesch G. 2003 “Modeling Engine Spray and Combustion Processes” Springer-Verlag Berlin Heidelberg AVL BOOST plc. 2013. AVL Software www.avl.com/BOOST.
 Emadi A. Ehsani M. 2000 “Aircraft power systems: technology state of the art and future trends” Aerosp Electron Syst Mag IEEE 15(1).
 Roboam X. 2011 “New trends and challenges of electrical networks embedded in “more electrical aircraft” Proceedings of 2011 IEEE International Symposium on Industrial Electronics (ISIE) pp. 26-31.
 Pietrykowski K. 2011 “Research on the mixture formation process in a radial engine” Combustion Engines PTNSS–2011–SC–015.
 Gęca M. Wendeker M. Litak G. 2012 “Combustion variability and uniqueness in cylinder of a large power radial engine Journal of Vibroengineering” Vol. 14 Issue 2. pp. 582-591.
 Grabowski Ł. Tulwin T. Geca M. and Karpiński P. 2016 “Validation Study of Radial Aircraft Engine Model” International Journal of Aerospace and Mechanical Engineering 9(3) pp. 2316-2316.
 Wendeker M. Kacejko P. Duk M. and Karpiński P. 2016 “Simulation Research of Innovative Ignition System of ASz62IR Radial Aircraft Engine” International Journal of Aerospace and Mechanical Engineering 9(3) pp. 2320-2320.
 Pietrykowski K. and Gęca M. 2014 „Simulation studies of the aircraft radial engine” (in Polish: “Badania symulacyjne lotniczego silnika gwiazdowego”) Logistyka 6/2014.
 Magryta P. Tulwin T. and Karpiński P. 2016 “The Charge Exchange and Mixture Formation Model in the ASz-62IR Radial Aircraft Engine” International Journal of Aerospace and Mechanical Engineering 9(3) pp. 2319-2319.
 Duk M. Grabowski Ł. and Magryta P. 2016 “Operation Cycle Model of ASz62IR Radial Aircraft Engine” International Journal of Aerospace and Mechanical Engineering 9(3) pp. 2322-2322.