aircraft design

Feasibility and benefit assessments of hybrid hydrogen fuel cell and battery configurations on a regional turboprop aircraft
This paper explors different hybrid configurations and comparing their fuel burn benefits in an attempt to identify whether hybrid …
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Advanced 2030 turboprop aircraft modeling for the electrified powertrain flight demonstration program
Electrified aircraft propulsion concepts are rapidly emerging due to their huge potential in fuel saving and mitigating negative …
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Analysis of a Hybrid Partial Turboelectric Distributed Propulsion System for a Medium Altitude Long Endurance UAV
Electrified propulsion offers high efficiency, scalability, and high power discharge capability which can be utilized for increased …
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Finalized Design and Performance Analysis of a Hybrid Turbo-Electric Regional Jet for the NASA ULI Program
Under the NASA University Leadership Initiative (ULI) program, a team formed by multi-disciplinary universities are collaborating on …
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Modeling and Simulation of a Parallel Hybrid Electric Regional Aircraft for the Electrified Powertrain Flight Demonstration (EPFD) Program
2022 EATS Best Paper Award. This paper presents a parametric modeling and integrated sizing approach for a charge-depleting parallel …
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Viability Study of an Electrified Regional Turboprop
The growth in hydrocarbon emissions and greenhouse gases, created by the aviation industry, has led to the demand of multilateral …
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System Analysis and Design Space Exploration of Regional Aircraft with Electrified Powertrains
This paper explores the design spaces of a thin-haul and a regional aircraft with parallel hybrid electric propulsion architectures and …
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System Analysis and Design Space Exploration of Regional Aircraft with Electrified Powertrains
Fleet Analysis of a Hybrid Turboelectric Commercial Regional Jet under NASA ULI Program
Under the NASA University Leadership Initiative (ULI) program, researchers from multiple institutes are collaborating on development of …
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Performance Assessment of a Distributed Electric Propulsion System for a Medium Altitude Long Endurance Unmanned Aerial Vehicle
Distributed propulsion systems are enabled by electrified aircraft and can provide aero-propulsive benefits. The magnitude and impact …
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An Update on Sizing and Performance Analysis of a Hybrid Turboelectric Regional Jet for the NASA ULI Program
Under the NASA University Leadership Initiative (ULI) program, a team of universities are collaborating on the advancement of …
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