Parallel Hybrid Gas-Electric Geared Turbofan Engine Conceptual Design and Benefits Analysis-Reference-Cited by-同舟云学术

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

Published:2016-07-22 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
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Author:

Lents Charles E.,Hardin Larry W.,Rheaume Jonathon,Kohlman Lee

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4610

Reference5 articles.

1. 1Bradley, M. K., and Droney, C. K. "Subsonic Ultra Green Aircraft Research Phase I Final Report," National Aeronautics and Space Administration Contractor Report NASA/CR-2011-216847, 2011.

2. 2Bradley, M. K., and Droney, C. K. "Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development," National Aeronautics and Space Administration Contractor Report NASA/CR-2012-217556, 2012.

3. Conceptual Design of a Single-Aisle Turboelectric Commercial Transport with Fuselage Boundary Layer Ingestion

4. Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements

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