Title:
Uncertainty Quantification of a Parallel Hybrid-Electric Propulsion EPFD Vehicle

dc.contributor.author Uzodinma, Jaylon
dc.contributor.author Zaidi, Turab
dc.contributor.author Walter, Miguel
dc.contributor.author Gautier, Raphael
dc.contributor.author Mavris, Dimitri N.
dc.contributor.corporatename Georgia Institute of Technology. Aerospace Systems Design Laboratory en_US
dc.contributor.corporatename American Institute of Aeronautics and Astronautics
dc.contributor.corporatename Georgia Institute of Technology. Aerospace Systems Design Laboratory
dc.date.accessioned 2023-02-03T15:44:19Z
dc.date.available 2023-02-03T15:44:19Z
dc.date.issued 2023-01
dc.description Presented at the American Institute of Aeronautics and Astronautics (AIAA) SciTech 2023 Forum en_US
dc.description.abstract The NASA Electrified Powertrain Flight Demonstration (EPFD) program is a collaboration between industry and academia to accelerate the development and implementation of megawatt-class power systems in commercial aviation. Technology development programs are often associated with cost, performance, and schedule risks, which can result from technical uncertainty. To assess and offer insight to effective mitigation of risks associated with the NASA EPFD program, an uncertainty quantification analysis for future hybrid-electric commercial aircraft is addressed. An uncertainty analysis is presented for the electrified aircraft propulsion systems of a 150-passenger hybrid-electric aircraft model. Uncertainty at the component-level of the powertrain system is considered and its effect is propagated to vehicle-level metrics. The primary focus is identifying and assessing the key uncertain technological inputs driving the variability of the vehicle’s performance responses. en_US
dc.description.sponsorship National Aeronautics and Space Administration (NASA) WD-002344 (NIA-602015) en_US
dc.identifier.citation Jaylon Uzodinma, Turab Zaidi, Miguel Walter, Raphael Gautier and Dimitri N. Mavris. "Uncertainty Quantification on a Parallel Hybrid-Electric Propulsion EPFD Vehicle," AIAA 2023-0839. AIAA SCITECH 2023 Forum. January 2023. DOI: https://doi.org/10.2514/6.2023-0839 en_US
dc.identifier.doi https://doi.org/10.2514/6.2023-0839 en_US
dc.identifier.uri http://hdl.handle.net/1853/70261
dc.language.iso en_US en_US
dc.publisher AIAA en_US
dc.publisher Georgia Institute of Technology
dc.publisher.original American Institute of Aeronautics and Astronautics (AIAA)
dc.relation.ispartofseries ASDL;
dc.relation.ispartofseries ASDL; AIAA
dc.subject Uncertainty quantification en_US
dc.subject Hybrid-Electric Propulsion en_US
dc.subject Aircraft design en_US
dc.subject Sustainability en_US
dc.subject Electrified aircraft en_US
dc.title Uncertainty Quantification of a Parallel Hybrid-Electric Propulsion EPFD Vehicle en_US
dc.type Text
dc.type.genre Paper
dspace.entity.type Publication
local.contributor.author Mavris, Dimitri N.
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.contributor.corporatename Aerospace Systems Design Laboratory (ASDL)
local.contributor.corporatename College of Engineering
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relation.isOrgUnitOfPublication a8736075-ffb0-4c28-aa40-2160181ead8c
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
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