@inproceedings{8974e55384cb458290d25bbcef18b739,
title = "A computational model for the study of gas turbine combustofcdynamics",
abstract = "A dynamic combustor model is developed for inclusion into a one-dimensional full gas turbine engine simulation code. A fluxdifference splitting algorithm is used to numerically integrate the quasi-one-dimensional Euler equations, supplemented with species mass conservation equations. The combustion model involves a single-step, global finite-rate chemistry scheme with a temperaturedependent activation energy. Source terms are used to account for mass bleed and mass injection, with additional capabilities to handle momentum and energy sources and sinks. Numerical results for cold and reacting flow for a can-type gas turbine combustor are presented. Comparisons with experimental data from this combustor are also made.",
author = "Costura, {David M.} and Lawless, {Patrick B.} and Frankel, {Steven H.}",
note = "Publisher Copyright: Copyright {\textcopyright} 1998 by ASME.; ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1998 ; Conference date: 02-06-1998 Through 05-06-1998",
year = "1998",
doi = "10.1115/98-GT-342",
language = "אנגלית",
series = "Proceedings of the ASME Turbo Expo",
booktitle = "Aircraft Engine; Marine; Microturbines and Small Turbomachinery",
}