Aero-Propulsive and Aero-Structural Design Integration of Turboprop Aircraft with Electric Wingtip-Mounted Propellers
Author:
Affiliation:
1. Technische Universiteit Delft
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0167
Reference27 articles.
1. Propeller-wing integration for minimum induced loss
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4. Wingtip-Mounted Propellers: Aerodynamic Analysis of Interaction Effects and Comparison with Conventional Layout
5. Veldhuis, L.L.M. “Propeller Wing Aerodynamic Interference,” Ph.D. thesis,Delft University of Technology, Jun. 2005. URL http://resolver.tudelft.nl/uuid:8ffbde9c-b483-40de-90e0-97095202fbe3.
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1. Rapid Aerostructural Optimization of Wing-Propeller Systems;AIAA SCITECH 2024 Forum;2024-01-04
2. Dual-Solver Hybrid Computational Approach to Integrated Propulsion Aerodynamics;Journal of Aircraft;2023-03
3. Distributed Hybrid-Electric Propulsion Benefits for Span-Limited Aircraft;AIAA SCITECH 2023 Forum;2023-01-19
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