Aeropropulsive Coupling Effects on a General-Aviation Aircraft with Distributed Electric Propulsion-Reference-Cited by-同舟云学术

Aeropropulsive Coupling Effects on a General-Aviation Aircraft with Distributed Electric Propulsion

Published:2021-11 Issue:6 Volume:58 Page:1351-1363
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Perry Aaron T.¹,Bretl Timothy¹,Ansell Phillip J.¹

Affiliation:

1. University of Illinois at Urbana-Champaign, Urbana, IL 61801

Funder

NASA STTR

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036048

Reference35 articles.

1. WadelM.FernandezH.AndersS. “Advanced Air Transport Technology (AATT),” NASA GRC-E-DAA-TN72727, Aug. 2019.

2. Mission Analysis and Emissions for Conventional and Hybrid-Electric Regional Jet Aircraft

3. FelderJ. L.BrownG. V.KimH. D.ChuJ., Turboelectric Distributed Propulsion in a Hybrid Wing Body Aircraft,” International Society for Air Breathing Engines, Paper ISABE-2011-1340, 2011.

4. Trade Studies for NASA N3-X Turboelectric Distributed Propulsion System Electrical Power System Architecture

5. A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology

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