This thesis describes and evaluates experiments conducted on a rotor test facility with a focus on blade tip vortices. The flow field of a four-bladed rotor was studied with the particle image velocimetry (PIV) method to visualise the flow field. The experimental setup and procedure is described in detail as well as the computer based evaluation techniques. Interesting vortex interaction is discovered and interaction and vortex parametres are studied when varying parametres such as blade angle of incidence and axial inflow speed. A basic understanding of blade tip interaction for the test facility is gained and experimental data for future investigations is gathered. Vortex interaction is found to occur when axial inflow is sufficiently...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
The interaction of a helicopter tail rotor blade with the tip vortex system from the main rotor is a...
The blade-tip vortex of a rotating and pitching DSA-9A blade was investigated numerically and experi...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
The aerodynamic operating conditions of a propeller can include complex situations where vorticity f...
The complex flowfield which is associated with a rotor wake gives rise to the multitude of aerodynam...
To characterize the vortex system of a helicopter rotor with cyclic pitch, an experimental investiga...
International audienceThis paper presents the results of an experimental study of two closely spaced...
An investigation into blade tip vortices of a sub-scale rotor under cyclic pitch conditions is carri...
The tip vortex system downstream of a four-bladed instrumented rotor was investigated experimentally...
The flow field around a helicopter is dominated by strong coherent vortices originating from the bla...
In order to investigate the development of blade tip vortices under different rotor conditions like ...
The tip vortex of a wind turbine rotor blade originates as a result of a complex distribution of vor...
The vortex system of four rotating and pitching DSA-9A blades was examined numerically and experimen...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
The interaction of a helicopter tail rotor blade with the tip vortex system from the main rotor is a...
The blade-tip vortex of a rotating and pitching DSA-9A blade was investigated numerically and experi...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
The aerodynamic operating conditions of a propeller can include complex situations where vorticity f...
The complex flowfield which is associated with a rotor wake gives rise to the multitude of aerodynam...
To characterize the vortex system of a helicopter rotor with cyclic pitch, an experimental investiga...
International audienceThis paper presents the results of an experimental study of two closely spaced...
An investigation into blade tip vortices of a sub-scale rotor under cyclic pitch conditions is carri...
The tip vortex system downstream of a four-bladed instrumented rotor was investigated experimentally...
The flow field around a helicopter is dominated by strong coherent vortices originating from the bla...
In order to investigate the development of blade tip vortices under different rotor conditions like ...
The tip vortex of a wind turbine rotor blade originates as a result of a complex distribution of vor...
The vortex system of four rotating and pitching DSA-9A blades was examined numerically and experimen...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
The interaction of a helicopter tail rotor blade with the tip vortex system from the main rotor is a...
The blade-tip vortex of a rotating and pitching DSA-9A blade was investigated numerically and experi...