Aerodynamic design modification of the Kopter AW09 helicopter

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dc.contributor.authorRess, R.
dc.contributor.authorPulfer, M.
dc.contributor.authorHirsch, F.
dc.contributor.authorKummel, A.
dc.contributor.authorBreitsamter, C.
dc.date.accessioned2024-12-12T18:47:34Z
dc.date.available2024-12-12T18:47:34Z
dc.date.issued2021
dc.description.abstractWind tunnel testing and accompanying numerical analyses are the basic methods applied to improve and optimize the aerodynamic design of the Kopter AW09, a 2.8 ton-class single engine utility helicopter. In order to ensure good handling qualities and performance, modifications of the upper fuselage are tested and evaluated by means of force and moment measurements, particle image velocimetry, and CFD analysis. Based on particular examples, these methods are presented.
dc.identifier.otherERF-2021-064
dc.identifier.urihttps://hdl.handle.net/20.500.11881/4252
dc.language.isoen
dc.titleAerodynamic design modification of the Kopter AW09 helicopter

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