Development of Turboelectric Propulsion and Power for Small Unmanned Aircraft-Reference-Cited by-同舟云学术

Development of Turboelectric Propulsion and Power for Small Unmanned Aircraft

Published:2018-07-08 Issue: Volume: Page:
ISSN:
Container-title:2018 Joint Propulsion Conference
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Author:

Rouser Kurt P.¹,Lucido Nicholas¹,Durkee Matthew¹,Bellcock Andrew¹,Zimbelman Tyler¹

Affiliation:

1. Oklahoma State University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4618

Reference12 articles.

1. Moving towards a more electric aircraft

2. More Electric Aircraft: Review, Challenges, and Opportunities for Commercial Transport Aircraft

3. Turboelectric Distributed Propulsion Engine Cycle Analysis for Hybrid-Wing-Body Aircraft

4. Weights and Efficiencies of Electric Components of a Turboelectric Aircraft Propulsion System

5. 8K. McKinney, "Evaluation of Hybrid-Electric Power System Integration Challenges for Multi-Rotor UAS," MS Thesis,Oklahoma State University, Schoolof Mechanical and Aerospace Engineering,2018.

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3. Validation of Analytical Model for Turboelectric Power System for Preliminary Design Purposes;Journal of Engineering for Gas Turbines and Power;2020-08-01

4. Design, Characterization, and Integration of a Turboelectric Power System for Small Unmanned Multirotor Aircraft;AIAA Propulsion and Energy 2019 Forum;2019-08-16

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