Pylon Design for a Short Range Transport Aircraft with Over-the-Wing Mounted UHBR Engines
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0011
Reference14 articles.
1. Aerodynamic Installation Effects of an Over-the-Wing Propeller on a High-Lift Configuration
2. Over Wing Nacelle Installations for Improved Energy Efficiency
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