Add to ORKGThe following report details the current investigation into the behaviour of the vortex core axial flow during the BVI, highlighting the salient features promoted by the interaction. The feasibility of acquiring PIV and pressure data simultaneously for the orthogonal BVI has also been examined
This dissertation describes an experimental investigation of the blade-vortex interaction (BVI) phen...
Transonic perpendicular rotor blade-vortex interaction (BVI) tests at Mach numbers ranging from 0.68...
In some situations, concentrated vorticity which forms a vortical flow is involved in the inflow of ...
The following report details the current investigation into the behaviour of the vortex core axial f...
Preliminary results from a PIV study of the orthogonal blade-vortex interaction are presented. The t...
Preliminary results from a PIV study of the orthogonal blade-vortex interaction are presented. This ...
The complex flowfield which is associated with a rotor wake gives rise to the multitude of aerodynam...
Wind-tunnel tests were conducted to investigate orthogonalvortex interaction with a stationary blade...
An orthogonal blade–vortex interaction has been visualised using stereo particle image velocimetry. ...
Rotors of vertical take-off and landing vehicles (main rotor, tail rotor, and propeller) are often s...
© American Institute of Aeronautics and AstronauticsA unique vortex generator that simulates the tra...
Steps towards the implementation of a stereoscopic particle image velocimetry (PIV) system for the i...
A comprehensive study on vortex dynamics during parallel blade-vortex interaction (BVI) was conducte...
Steps towards the implementation of a stereoscopic particle image velocimetry (PIV) system for the ...
The aerodynamic operating conditions of a propeller can include complex situations where vorticity f...
This dissertation describes an experimental investigation of the blade-vortex interaction (BVI) phen...
Transonic perpendicular rotor blade-vortex interaction (BVI) tests at Mach numbers ranging from 0.68...
In some situations, concentrated vorticity which forms a vortical flow is involved in the inflow of ...
The following report details the current investigation into the behaviour of the vortex core axial f...
Preliminary results from a PIV study of the orthogonal blade-vortex interaction are presented. The t...
Preliminary results from a PIV study of the orthogonal blade-vortex interaction are presented. This ...
The complex flowfield which is associated with a rotor wake gives rise to the multitude of aerodynam...
Wind-tunnel tests were conducted to investigate orthogonalvortex interaction with a stationary blade...
An orthogonal blade–vortex interaction has been visualised using stereo particle image velocimetry. ...
Rotors of vertical take-off and landing vehicles (main rotor, tail rotor, and propeller) are often s...
© American Institute of Aeronautics and AstronauticsA unique vortex generator that simulates the tra...
Steps towards the implementation of a stereoscopic particle image velocimetry (PIV) system for the i...
A comprehensive study on vortex dynamics during parallel blade-vortex interaction (BVI) was conducte...
Steps towards the implementation of a stereoscopic particle image velocimetry (PIV) system for the ...
The aerodynamic operating conditions of a propeller can include complex situations where vorticity f...
This dissertation describes an experimental investigation of the blade-vortex interaction (BVI) phen...
Transonic perpendicular rotor blade-vortex interaction (BVI) tests at Mach numbers ranging from 0.68...
In some situations, concentrated vorticity which forms a vortical flow is involved in the inflow of ...