Two Aerodynamic Mid-Fidelity Approaches on a Distributed Propulsion Wing
Author:
Affiliation:
1. Rolls-Royce Deutschland Limited and Company KG, 81739 Munich, Germany
2. DLR, German Aerospace Center, 38108 Brunswick, Germany
3. Technical University of Munich, 80333 Munich, Germany
Abstract
Funder
LuFo V-3
LuFo VI-1
LuFo VI-2
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C037313
Reference54 articles.
1. Distributed Electric Propulsion Effects on Existing Aircraft Through Multidisciplinary Optimization
2. Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight
3. Towards higher aerodynamic efficiency of propeller-driven aircraft with distributed propulsion
4. VeldhuisL. L. M. “Propeller Wing Aerodynamic Interference,” Ph.D. Dissertation, Delft Univ. of Technology, Delft, The Netherlands, June 2005, http://resolver.tudelft.nl/uuid:8ffbde9c-b483-40de-90e0-97095202fbe3 [retrieved 1 Sept. 2022].
5. PrandtlL. “Mutual Influence of Wings and Propeller,” Extract from the First Report of the Göttingen Aerodynamics Lab. NACA TN 74, 1921, https://ntrs.nasa.gov/citations/19930080882 [retrieved 1 Sept. 2022].
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