Comparison of Aero-Propulsive Performance Predictions for Distributed Propulsion Configurations
Author:
Affiliation:
1. NASA Langley Research Center
2. Joby Aviation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0209
Reference46 articles.
1. Effects of wingtip-mounted propellers on wing lift and induced drag.
2. High-Lift Propulsive Airfoil with Integrated Crossflow Fan
3. Wake ingestion propulsion benefit
4. Conceptual Design of a Single-Aisle Turboelectric Commercial Transport with Fuselage Boundary Layer Ingestion
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