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Comparison of the results of mathematical modeling of a GTM 120 miniature turbine jet engine with the research results
1
Faculty of Mechatronics and Aeronautics, Military University of Technology, Warsaw.
2
Faculty of Power and Aeronautical Engineering, Warsaw University of Technology.
3
Faculty of Mechanical Engineering, Łódz University of Technology.
Publication date: 2018-05-01
Combustion Engines 2018,173(2), 30-33
KEYWORDS
ABSTRACT
The paper presents gas-dynamic calculations of a GTM 120 miniature turbine jet engine. The engine performance parameters have been determined and then validated with theory contained in literature as well as the results of research carried out on a laboratory test stand.
REFERENCES (8)
1.
CICHOSZ, E., KORDZIŃSKI, W., ŁYŻWIŃSKI, M. et al. Napędy lotnicze. Charakterystyka i zastosowanie. Warsza-wa: WKiŁ 1980.
2.
DZIERŻANOWSKI, P., KORDZIŃSKI, W., ŁYŻWIŃSKI, M. et al. Turbinowe silniki odrzutowe. Warszawa, WKiŁ 1983.
3.
DZIERŻANOWSKI, P., OTYŚ, J., SZCZECIŃSKI, S. et al. Konstrukcja silników lotniczych. Projektowanie przejściowe i dyplomowe. Warszawa, Wydział Wydawniczy WAT 1972.
4.
GIERAS, M. Miniaturowe silniki turboodrzutowe. Warsza-wa, Oficyna Wydawnicza Politechniki Warszawskiej 2016.
5.
KAU, H-K. Optimization of a model jet engine. Institute of Flight Propulsion, Technische Universitat Munchen 2009.
6.
TRZECIAK, A. Odtworzenie parametrów obiegu i wyznaczenie osiągów i charakterystyk turbinowego silnika odrzutowego GTM 120. Praca dyplomowa. WAT Warszawa 2012.
CITATIONS (3):
1.
Model-based dynamic performance simulation of a microturbine
Mario Erario, Giorgi De, Radoslaw Przysowa
IOP Conference Series: Materials Science and Engineering
Mario Erario, Giorgi De, Radoslaw Przysowa
IOP Conference Series: Materials Science and Engineering
2.
Model-Based Dynamic Performance Simulation of a Microturbine Using Flight Test Data
Mario Erario, Giorgi De, Radoslaw Przysowa
Aerospace
Mario Erario, Giorgi De, Radoslaw Przysowa
Aerospace
3.
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