Multi-Point Design of Parallel Hybrid Aero Engines-Reference-Cited by-同舟云学术

Multi-Point Design of Parallel Hybrid Aero Engines

Published:2020-08-17 Issue: Volume: Page:
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Container-title:AIAA Propulsion and Energy 2020 Forum
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Author:

Sielemann Michael¹,Coïc Clément¹,Zhao Xin²,Diamantidou Dimitra Eirini³,Kyprianidis Konstantinos³

Affiliation:

1. Modelon

2. Chalmers University of Technology

3. Mälardalen University

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. Overview of NASA Electrified Aircraft Propulsion (EAP) Research for Large Subsonic Transports

2. Bradley, M. K., and Droney, C. K. “Subsonic ultra green aircraft research,” Contractor Report NASA/CR-2011-216847, NASA Langley Research Center, Hampton, VA, 2011.

3. Bradley, M. K., and Droney, C. K. “Subsonic Ultra Green Aircraft Research Phase II: Hybrid Electric Design Exploration,” Contractor Report NASA/CR-2015-218704/Volume II, NASA Langley Research Center, Hampton, VA, 2015.

4. Parallel Hybrid Gas-Electric Geared Turbofan Engine Conceptual Design and Benefits Analysis

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3. Exploring Design Trade-Offs For Installed Parallel Hybrid Powertrain Systems;AIAA Propulsion and Energy 2021 Forum;2021-07-28

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