Initial Sizing Methodology for Hybrid-Electric General Aviation Aircraft-Reference-Cited by-同舟云学术

Initial Sizing Methodology for Hybrid-Electric General Aviation Aircraft

Published:2020-03 Issue:2 Volume:57 Page:245-255
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Finger D. Felix¹,Bil Cees¹,Braun Carsten²

Affiliation:

1. RMIT University, Melbourne, Victoria 3083, Australia

2. FH Aachen University of Applied Sciences, 52064 Aachen, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference20 articles.

1. HepperleM. “Electric Flight—Potential and Limitations,” NATO MP-AVT-209-09, Energy Efficient Technologies and Concepts of Operation, Lisbon, Portugal, Oct. 2012.

2. MooreM. D.FredericksB. “Misconceptions of Electric Propulsion Aircraft and Their Emergent Aviation Markets,” AIAA Paper 2014-0535, 2014. 10.2514/6.2014-0535

3. Aircraft Engine Design, Second Edition

4. LoftinL. K. Jr. “Subsonic Aircraft: Evolution and the Matching of Size to Performance,” NASA Langley Research Center, NASA-RP-1060, 1980, https://ntrs.nasa.gov/search.jsp?R=19800020744.

5. Aircraft Design: A Conceptual Approach, Sixth Edition

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