Pylon trailing edge blowing was investigated as a means of alleviating the effects of the pylon wake on a pusher arrangement of an advanced single-rotation turboprop. Measurements were made of steady-state propeller thrust and pylon wake pressures and turbulence levels with and without blowing. Results show that the pylon trailing edge blowing practically eliminated the pylon wake, significantly reduced the pylon wake turbulence, and had a relatively small effect on the steady-state propeller thrust. The data are presented with a minimum of analysis
An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of a...
The present study represents an extension of an earlier wind tunnel experiment performed with the P&...
Results of a parametric study to determine the effects of design variables and penalties on the fuel...
This paper presents an experimental assessment of the working principles of pylon trailing-edge blow...
Advanced propellers promise significant fuel-burn savings compared to turbofans. When installed on t...
Pylon-mounted pusher propellers suffer from installation effects due to the interaction between the ...
This report discusses the potential of pylon trailing edge blowing to reduce the adverse effects of ...
An experimental investigation was performed at the Large Low-speed Facility of the German-Dutch wind...
International audienceThe aerodynamic impact of installing a horizontal pylon in front of a contra-r...
Open rotors are considered to have the potential to improve the fuel economy of aircraft significant...
Advanced propeller propulsion systems potentially provide a significant reduction in fuel burn compa...
The flow field between a model empennage and a 591-mm-diameter pusher propeller was studied in the A...
An experimental analysis was performed of the unsteady aerodynamic loading caused by the impingement...
The impingement of a propeller slipstream on a downstream surface causes unsteady loading, which may...
Experimental and analytical effort shows that use of advanced turboprop (propfan) propulsion instead...
An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of a...
The present study represents an extension of an earlier wind tunnel experiment performed with the P&...
Results of a parametric study to determine the effects of design variables and penalties on the fuel...
This paper presents an experimental assessment of the working principles of pylon trailing-edge blow...
Advanced propellers promise significant fuel-burn savings compared to turbofans. When installed on t...
Pylon-mounted pusher propellers suffer from installation effects due to the interaction between the ...
This report discusses the potential of pylon trailing edge blowing to reduce the adverse effects of ...
An experimental investigation was performed at the Large Low-speed Facility of the German-Dutch wind...
International audienceThe aerodynamic impact of installing a horizontal pylon in front of a contra-r...
Open rotors are considered to have the potential to improve the fuel economy of aircraft significant...
Advanced propeller propulsion systems potentially provide a significant reduction in fuel burn compa...
The flow field between a model empennage and a 591-mm-diameter pusher propeller was studied in the A...
An experimental analysis was performed of the unsteady aerodynamic loading caused by the impingement...
The impingement of a propeller slipstream on a downstream surface causes unsteady loading, which may...
Experimental and analytical effort shows that use of advanced turboprop (propfan) propulsion instead...
An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine the effects of a...
The present study represents an extension of an earlier wind tunnel experiment performed with the P&...
Results of a parametric study to determine the effects of design variables and penalties on the fuel...