Experiments were performed where a blade of symmetrical pro le was placed one chord upstream of another blade of identical dimensions but installed with miniature pressure transducers around the chord. The purpose of such a test was to simulate the e ect of multiple orthogonal vortex interactions which may occur within the tail rotors of helicopters. It was found that when the upstream blade was installed, the pressure response experienced by the instrumented blade was similar in form but reduced in magnitude by 50% compared with results obtained without the upstream blade. This indicates that the vortex has the ability to reconnect and re-establish rotational and axial components after an initial cut. It also implies that noise and vibrati...
The aeroacoustic response of the orthogonal interaction of a rotating blade with an isolated Batchel...
Numerical investigations of helicopter blade-vortex mechanism of interaction are performed using lar...
This paper presents and provides analysis of unsteady surface pressures measured on a model rotor bl...
The interaction of a helicopter tail rotor blade with the tip vortex system from the main rotor is a...
Wind-tunnel tests were conducted to investigate orthogonalvortex interaction with a stationary blade...
A unique and novel experimental approach has been developed to study the aerodynamics and acoustics ...
A unique and novel experimental approach has been developed to study the aerodynamics and acoustics ...
© American Institute of Aeronautics and AstronauticsA unique vortex generator that simulates the tra...
International audienceThis paper presents the results of an experimental study of two closely spaced...
Preliminary results from a PIV study of the orthogonal blade-vortex interaction are presented. This ...
The interaction of a helicopter’s main rotor tip vortex with the tail rotor is an important source o...
Activities carried out in support of research on flow structure generated by perpendicular blade vor...
Preliminary results from a PIV study of the orthogonal blade-vortex interaction are presented. The t...
This dissertation describes an experimental investigation of the blade-vortex interaction (BVI) phen...
Understanding the mechanisms that lead to the production of noise by tail rotors across a broad rang...
The aeroacoustic response of the orthogonal interaction of a rotating blade with an isolated Batchel...
Numerical investigations of helicopter blade-vortex mechanism of interaction are performed using lar...
This paper presents and provides analysis of unsteady surface pressures measured on a model rotor bl...
The interaction of a helicopter tail rotor blade with the tip vortex system from the main rotor is a...
Wind-tunnel tests were conducted to investigate orthogonalvortex interaction with a stationary blade...
A unique and novel experimental approach has been developed to study the aerodynamics and acoustics ...
A unique and novel experimental approach has been developed to study the aerodynamics and acoustics ...
© American Institute of Aeronautics and AstronauticsA unique vortex generator that simulates the tra...
International audienceThis paper presents the results of an experimental study of two closely spaced...
Preliminary results from a PIV study of the orthogonal blade-vortex interaction are presented. This ...
The interaction of a helicopter’s main rotor tip vortex with the tail rotor is an important source o...
Activities carried out in support of research on flow structure generated by perpendicular blade vor...
Preliminary results from a PIV study of the orthogonal blade-vortex interaction are presented. The t...
This dissertation describes an experimental investigation of the blade-vortex interaction (BVI) phen...
Understanding the mechanisms that lead to the production of noise by tail rotors across a broad rang...
The aeroacoustic response of the orthogonal interaction of a rotating blade with an isolated Batchel...
Numerical investigations of helicopter blade-vortex mechanism of interaction are performed using lar...
This paper presents and provides analysis of unsteady surface pressures measured on a model rotor bl...