Methodology for Sizing and Performance Assessment of Hybrid Energy Aircraft-Reference-Cited by-同舟云学术

Methodology for Sizing and Performance Assessment of Hybrid Energy Aircraft

Published:2015-01 Issue:1 Volume:52 Page:341-352
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Pornet C.¹,Gologan C.¹,Vratny P. C.¹,Seitz A.¹,Schmitz O.¹,Isikveren A. T.¹,Hornung M.¹

Affiliation:

1. Research and Technology, Bauhaus Luftfahrt e.V., 80807 Munich, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032716

Reference23 articles.

1. BradleyM. K.DroneyC. K. “Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development,” NASA CR-2012-217556, Huntington Beach, CA, 2012.

2. BrunerS.BaberS.HarrisC.CaldwellN.KedingP.RahrigK.PhoL.WlezianR. “NASA N+3 Subsonic Fixed Wing Silent Efficient Low-Emissions Commercial Transport (SELECT) Vehicle Study,” NASA CR-2010-216798, El Segundo, CA, 2010.

3. BradleyM. K.DroneyC. K. “Subsonic Ultra Green Aircraft Research: Phase I Final Report,” NASA CR-2011-216847, Huntington Beach, CA, 2011.

4. A Generalized Aircraft Sizing Method and Application to Electric Aircraft

5. Power Based Sizing Method for Aircraft Consuming Unconventional Energy

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