Integrated Aerodynamic Benefits of Distributed Propulsion
Author:
Affiliation:
1. Lockheed Martin Corporation
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1500
Reference15 articles.
1. Over Wing Nacelle Installations for Improved Energy Efficiency
2. The Potential and Challenge of TurboElectric Propulsion for Subsonic Transport Aircraft
3. Split-Wing Propulsor Design and Analysis for Electric Distributed Propulsion
4. Analysis of a Distributed Hybrid Propulsion System with Conventional Electric Machines
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