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Titel:

TRANSPORT AIRCRAFT WING INVESTIGATIONS AIMED ON WAKE VORTEX IMPACT BY OSCILLATING FLAPS

Dokumenttyp:
Konferenzbeitrag
Art des Konferenzbeitrags:
Textbeitrag / Aufsatz
Autor(en):
Ruhland J.; Heckmeier F.M.; Breitsamter C.
Abstract:
The effect of oscillating trailing edge flaps on the wake vortex system of a generic transport aircraft is investigated. The half model presents a high lift configuration (droop nose, advanced dropped hinge flaps) of a generic transport aircraft. For constant temperature anemometry (CTA) measurements, experiments are carried out in the Göttingen-type low-speed wind tunnel C of the Chair of Aerodynamics and Fluid Mechanics of the Technical University of Munich. The experiments are performed at lo...     »
Stichworte:
Constant temperature anemometry; Dynamic flap motion; Wake vortex system analysis
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
International Council of the Aeronautical Sciences
Kongress / Zusatzinformationen:
32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021Shanghai, 6 September 2021 through 10 September 2021, Code 176566
Jahr:
2022
Nachgewiesen in:
Scopus
Print-ISBN:
978-393218291-4
Sprache:
en
Hinweise:
Funding text: The funding of this investigation within the LUFO V3 project BIMOD (FKZ: 20E1702C) by the German Federal Ministry for Economic Affairs and Energy (BMWi), is gratefully acknowledged.
TUM Einrichtung:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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