Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Michael J. Broomhead"'
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
Real-time simulation of gas turbine engine performance is used in a variety of aerospace applications. For simulation of propulsion system performance in flight-simulators, fidelity requirements become increasingly stringent. Significant improvements
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d9db65b70adf199ac90188cdb74b2fd2
https://doi.org/10.1115/2001-gt-0446
https://doi.org/10.1115/2001-gt-0446
Autor:
Michael J. Broomhead, W. P. J. Visser
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
NLR’s primary tool for gas turbine engine performance analysis is the ‘Gas turbine Simulation Program’ (GSP), a component based modeling environment. GSP’s flexible object-oriented architecture allows steady-state and transient simulation of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c94b6f62cedcdc7d9f3e33a67e78cf23
https://doi.org/10.1115/2000-gt-0002
https://doi.org/10.1115/2000-gt-0002
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
A method to predict gas turbine component life based on analysis of engine performance is presented. Engine performance history is obtained from in-flight monitored engine parameters and flight conditions and downloaded for processing by a tool integ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::42e13de575d6a9073f6e86b5d45b1752
https://doi.org/10.1115/2000-gt-0646
https://doi.org/10.1115/2000-gt-0646