Analysis of a Hybrid Partial Turboelectric Distributed Propulsion System for a Medium Altitude Long Endurance UAV-Reference-Cited by-同舟云学术

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Analysis of a Hybrid Partial Turboelectric Distributed Propulsion System for a Medium Altitude Long Endurance UAV

Published:2022-06-15 Issue: Volume: Page:
ISSN:
Container-title:2022 IEEE Transportation Electrification Conference & Expo (ITEC)
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Author:

Markov Alexander A.¹,Cinar Gokcin²,Brooks Joshua D.¹,Garcia Elena¹,Denney Russell K.¹,Mavris Dimitri N.¹,Patnaik Soumya S.³

Affiliation:

1. Georgia Institute of Technology,School of Aerospace Engineering,Atlanta,Georgia,30332

2. University of Michigan,Department of Aerospace Engineering,Ann Arbor,Michigan,48109

3. Air Force Research Laboratory,Aerospace Systems Directorate,Dayton,Ohio,45433

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9813698/9813746/09813926.pdf?arnumber=9813926

Reference8 articles.

1. Performance Assessment of a Distributed Electric Propulsion System for a Medium Altitude Long Endurance Unmanned Aerial Vehicle

2. Feasibility Assessments of a Hybrid Turboelectric Medium Altitude Long Endurance Unmanned Aerial Vehicle

3. Propeller design for conceptual turboprop aircraft;teeuwen;Master’s thesis,2017

4. Next Generation 2 MW Turboshaft and Turboprop Engines

5. Compact Heat Exchanger Sizing and Weight Estimation

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