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Titel:

Two Aerodynamic Mid-Fidelity Approaches on a Distributed Propulsion Wing

Dokumenttyp:
Zeitschriftenaufsatz
Autor(en):
Herzog, Nikolai; Keller, Dennis; Breitsamter, Christian
Abstract:
A comparison of two potential-theory based mid-fidelity approaches on the aerodynamics of a distributed propeller–wing tractor configuration is presented. The design space for aircraft configurations is enlarged by using distributed electric propulsion so a demand for investigating different variants, especially regarding the number of propellers, is present. While many lower fidelity tools are available in the literature, they are often only documented with integral results. This paper presents...     »
Dewey Dezimalklassifikation:
620 Ingenieurwissenschaften
Zeitschriftentitel:
Journal of Aircraft
Jahr:
2024
Band / Volume:
61
Heft / Issue:
1
Seitenangaben Beitrag:
196-210
Nachgewiesen in:
Scopus
Sprache:
en
Volltext / DOI:
doi:10.2514/1.c037313
Verlag / Institution:
American Institute of Aeronautics and Astronautics (AIAA)
E-ISSN:
0021-86691533-3868
Hinweise:
Acknowledgment: The authors acknowledge the financial support of the Federal Ministry for Economic Affairs and Climate Action under the framework of LuFo V-3 (FKZ:20A1706D), LuFo VI-1 (FKZ:20M1916A), and LuFo VI-2 (FKZ:20L2103A).
Eingereicht (bei Zeitschrift):
05.12.2022
Angenommen (von Zeitschrift):
21.08.2023
Publikationsdatum:
01.01.2024
TUM Einrichtung:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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