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Analysis and Optimization of Baseline Single Aisle Aircraft for Future Electrified Powertrain Flight Demonstrator ComparisonsThe purpose of this study is to provide baseline single-aisle vehicles for future comparisons NASA’s Electrified Powertrain Flight Demonstrator (EPFD) turbofan powered Vision Systems. Both a large single-aisle (≈150 passenger) and a small single-aisle (≈100 passenger) vehicle will be analyzed using NASA’s General Aviation Synthesis Program and a modernized Python-based version of this program that enables efficient gradient-based optimization of both the airframe and propulsion that currently is being referred to as GASPy. A technology build-up will be conducted to bring the current State-of-the-art vehicles to a projected 2035 technology level by incorporating estimations for improvements in aerodynamics, structures, and propulsions. These vehicles can be used in NASA’s future EPFD project as baselines to measure the benefits of future hybrid and fully electric aircraft against. The advanced, large single-aisle will then be used to demonstrate the benefits of a coupled engine-airframe optimization for fuel burn reduction.
Document ID
20220016441
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Carl J Recine
(Ames Research Center Mountain View, California, United States)
Dahlia D V Pham
(Ames Research Center Mountain View, California, United States)
Jeffrey V Bowles
(Ames Research Center Mountain View, California, United States)
Kenneth R Lyons
(Ames Research Center Mountain View, California, United States)
Benjamin W L Margolis
(Ames Research Center Mountain View, California, United States)
Joseph A Garcia
(Ames Research Center Mountain View, California, United States)
Date Acquired
October 31, 2022
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: AIAA/IEEE Electric Aircraft Technologies Symposium (EATS)
Location: San Diego, CA
Country: US
Start Date: June 12, 2023
End Date: June 16, 2023
Sponsors: American Institute of Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: 770848.06.01.10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
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