Modeling and Design of a Partially Electric Distributed Aircraft Propulsion System with GT-HEAT-Reference-Cited by-同舟云学术

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Modeling and Design of a Partially Electric Distributed Aircraft Propulsion System with GT-HEAT

Published:2017-01-05 Issue: Volume: Page:
ISSN:
Container-title:55th AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Gladin Jonathan C.¹,Trawick David¹,Perullo Christopher¹,Tai Jimmy C.¹,Mavris Dimitri N.¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1924

Reference25 articles.

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

2. "https://www.flightglobal.com/pdfarchive/view/1963/1963%20-%200476.html," [Online].

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