Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Metin F. Ozcan"'
Autor:
Jonathan C. Gladin, Cedric Y. Justin, Johannes A. Verberne, Metin F. Ozcan, Matilde D'Arpino, Francesco Porpora, Srujal Patel, Etienne Demers Bouchard
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fa405d830b07fd8860c52c5c03558c70
https://doi.org/10.2514/6.2021-3285
https://doi.org/10.2514/6.2021-3285
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f2828090a821b4a855352d9b427f5e0
https://doi.org/10.2514/6.2016-4639
https://doi.org/10.2514/6.2016-4639
Publikováno v:
16th AIAA Aviation Technology, Integration, and Operations Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d431c814dfe2ea2c762e765bb61ea2d1
https://doi.org/10.2514/6.2016-3146
https://doi.org/10.2514/6.2016-3146
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6fa5c406b4e80bec223f4e4106efd287
https://doi.org/10.2514/6.2015-4030
https://doi.org/10.2514/6.2015-4030
Publikováno v:
15th AIAA Aviation Technology, Integration, and Operations Conference.
The gas turbine engines on commercial aircraft produce both propulsive power and non-propulsive or secondary power for aircraft subsystems, which can be in the form of either pneumatic or mechanical power off-take. While there is a degradation in per
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::428193637178700bf98602bb93a37f0f
https://doi.org/10.2514/6.2015-3287
https://doi.org/10.2514/6.2015-3287
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Gas turbine engines are already complex and nonlinear systems. Nevertheless, gas turbines must become more complex and nonlinear over time to meet the more challenging requirements in the future. Consequently, the different gas turbine engine model t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e2bb17da9fbdc843607c8374c1a9124
https://doi.org/10.2514/6.2014-3928
https://doi.org/10.2514/6.2014-3928
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Modern civilian turbofans are complex and nonlinear systems, and they must get even more complex and nonlinear to meet the requirements for noise, emissions, and fuel burn in the future. The increase in the complexity and nonlinearity are due to more
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::912eb8b9d2c494f4fcd632bfc5b0d2ad
https://doi.org/10.2514/6.2013-4003
https://doi.org/10.2514/6.2013-4003
Autor:
Steven J. Sirica, Reza Rezvani, Dimitri N. Mavris, Richard P. Meisner, Metin F. Ozcan, Jimmy C. Tai, Brian K. Kestner
Publikováno v:
Volume 3: Controls, Diagnostics and Instrumentation; Education; Electric Power; Microturbines and Small Turbomachinery; Solar Brayton and Rankine Cycle.
This paper introduces a method to create engine transient models that retain the fidelity and non-linearity of complex models as well as simplicity and speed of lower fidelity linearized models. The method is based on the design of experiments (DOE)
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f7af63db0d059f853169c5a20b9d6fc
https://doi.org/10.1115/gt2011-45565
https://doi.org/10.1115/gt2011-45565