Experimental investigation of a rotor blade tip vortex pair - Archive ouverte HAL
Article Dans Une Revue CEAS Aeronautical Journal Année : 2022

Experimental investigation of a rotor blade tip vortex pair

Résumé

This paper presents the results of an experimental study of two closely spaced vortices generated by a rotating blade with a modified tip geometry. The experiments are carried out in two water channel facilities and involve a generic one-bladed rotor operating in a regime near hover. It is equipped with a parametric fin placed perpendicular to the pressure surface near the tip, which generates a co-rotating vortex pair having a helical geometry. Based on previous results obtained with a fixed wing, a series of small-scale experiments is first carried out, to validate the method of vortex pair generation also for a rotating blade, and to obtain a qualitative overview of its evolution going downstream. A more detailed quantitative study is then performed in a larger facility at three times the initial scale. By varying the fin parameters, it was possible to obtain a configuration in which the two vortices have almost the same circulation. In both experiments, the vortex pair is found to merge into a single helical wake vortex within one blade rotation. Particle image velocimetry measurements show that the resulting vortex has a significantly larger core radius than the single tip vortex from a blade without fin. This finding may have relevance in the context of blade-vortex interactions, where noise generation and fatigue from fluid-structure interactions depend strongly on the vortex core size.
Fichier principal
Vignette du fichier
Schröder_etal-CEAS-2021.pdf (4.3 Mo) Télécharger le fichier
Origine Fichiers éditeurs autorisés sur une archive ouverte

Dates et versions

hal-03431575 , version 1 (16-11-2021)

Identifiants

Citer

Dominic Schröder, Jorge Aguilar-Cabello, Thomas Leweke, Ralf Hörnschemeyer, Eike Stumpf. Experimental investigation of a rotor blade tip vortex pair. CEAS Aeronautical Journal, 2022, 13, pp.97-112. ⟨10.1007/s13272-021-00555-1⟩. ⟨hal-03431575⟩
50 Consultations
57 Téléchargements

Altmetric

Partager

More