Publication detail
Computational Model of Rotary Engine Thermodynamic Cycle
DRBAL, M.
English title
Computational Model of Rotary Engine Thermodynamic Cycle
Type
journal article - other
Language
en
Original abstract
During the engine prototype design period the performance predictions are the key subject of the development. For the piston reciprocating engines a wide spectrum of the analytical approaches was developed as well as the numerical software (GT-Suite, Ricardo Wave etc.) is being used often. The increasing demand for the high-power output engines with a low displacement and weight for the UAV and marine applications, makes Wankel rotary engine a sensible option. The commercially available software for the performance prediction does not include required algorithms for the rotary engine calculation. This paper provides an approach to be used in the simulation model setup as well as the comparison of the simulation outcome with the measured data.
English abstract
During the engine prototype design period the performance predictions are the key subject of the development. For the piston reciprocating engines a wide spectrum of the analytical approaches was developed as well as the numerical software (GT-Suite, Ricardo Wave etc.) is being used often. The increasing demand for the high-power output engines with a low displacement and weight for the UAV and marine applications, makes Wankel rotary engine a sensible option. The commercially available software for the performance prediction does not include required algorithms for the rotary engine calculation. This paper provides an approach to be used in the simulation model setup as well as the comparison of the simulation outcome with the measured data.
Keywords in English
rotary engine, engine performance prediction, 1D simulation
Released
26.06.2019
ISSN
1335-2393
Volume
23
Number
2
Pages from–to
26–29
Pages count
4
BIBTEX
@article{BUT164214,
author="Milan {Drbal},
title="Computational Model of Rotary Engine Thermodynamic Cycle",
year="2019",
volume="23",
number="2",
month="June",
pages="26--29",
issn="1335-2393"
}