Range Equation for Hybrid-Electric Aircraft with Constant Power Split-Reference-Cited by-同舟云学术

Range Equation for Hybrid-Electric Aircraft with Constant Power Split

Published:2020-05 Issue:3 Volume:57 Page:552-557
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

de Vries Reynard¹,Hoogreef Maurice F. M.¹,Vos Roelof¹

Affiliation:

1. Delft University of Technology, 2629 HS Delft, The Netherlands

Funder

European Union Horizon 2020 Program, as part of the Clean Sky 2 Program

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference38 articles.

1. BonetJ. T.SchellengerH. G.RawdonB. K.ElmerK. R.WakayamaS. R.BrownD. L.GuoY. “Environmentally Responsible Aviation (ERA) Project—N+2 Advanced Vehicle Concepts Study and Conceptual Design of Subscale Test Vehicle (STV): Final Report,” NASA CR-2011-216519, Dec. 2011.

2. Sizing of the energy storage system of hybrid-electric aircraft in general aviation

3. Mission Analysis and Component-Level Sensitivity Study of Hybrid-Electric General-Aviation Propulsion Systems

4. Benefit evaluation of hybrid electric propulsion concepts for CS-23 aircraft

5. Considerations for Reducing Aviation’s CO2 with Aircraft Electric Propulsion

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