In this work, computational fluid dynamics is used to compare experimental results for a two-bladed small rotor Out of Ground Effect and In Ground Effect conditions. The paper focuses on the evalutation and prediction of the performance of the rotor and investigates the outwash generated in ground effect. Time and phase averaged outflow velocities with two different scaling methods are compared with experiments. The results are also scaled to a full-size rotor, and compared with the PAXman model of crew operating in close rotor proximity. A particle pickup model is also used showing the dust cloud generated by the rotor
Downwash and outwash characteristics of a model-scale tandem-rotor system in the presence of the gro...
In this work, the ground effect phenomena for a rotary wing is investigated both numerically and exp...
In the present work, the aerodynamic performance of the full helicopter PSP in hover flight is inves...
In this work, computational fluid dynamics is used to compare experimental results for a two-bladed ...
n this work computational fluid dynamics is used to validate experimental results for a two-bladed s...
View Video Presentation: https://doi.org/10.2514/6.2021-2625.vid In this work, computational flui...
In this work, computational fluid dynamics was used to support safety analyses of rotors operating i...
In this work computational fluid dynamics is validated using experimental results for a model rotor ...
Computational fluid dynamics (CFD) is used here to predict the behaviour of ground particles, uplift...
A compressible, structured, overset Reynolds Averaged Navier Stokes (RANS) solver is used to simulat...
Quantitative and qualitative results of a series of experiments conducted on a rotor in ground effec...
The action of the rotor wake on loose sediment on the ground is primarily responsible for inducing t...
High-speed flow visualization and high-resolution particle image velocimetry experiments were conduc...
Rotorcraft operating in ground effect have been known to experience beneficial performance effects a...
In this work Computational Fluid Dynamics is used as a tool for rotor outwash evaluation. The paper ...
Downwash and outwash characteristics of a model-scale tandem-rotor system in the presence of the gro...
In this work, the ground effect phenomena for a rotary wing is investigated both numerically and exp...
In the present work, the aerodynamic performance of the full helicopter PSP in hover flight is inves...
In this work, computational fluid dynamics is used to compare experimental results for a two-bladed ...
n this work computational fluid dynamics is used to validate experimental results for a two-bladed s...
View Video Presentation: https://doi.org/10.2514/6.2021-2625.vid In this work, computational flui...
In this work, computational fluid dynamics was used to support safety analyses of rotors operating i...
In this work computational fluid dynamics is validated using experimental results for a model rotor ...
Computational fluid dynamics (CFD) is used here to predict the behaviour of ground particles, uplift...
A compressible, structured, overset Reynolds Averaged Navier Stokes (RANS) solver is used to simulat...
Quantitative and qualitative results of a series of experiments conducted on a rotor in ground effec...
The action of the rotor wake on loose sediment on the ground is primarily responsible for inducing t...
High-speed flow visualization and high-resolution particle image velocimetry experiments were conduc...
Rotorcraft operating in ground effect have been known to experience beneficial performance effects a...
In this work Computational Fluid Dynamics is used as a tool for rotor outwash evaluation. The paper ...
Downwash and outwash characteristics of a model-scale tandem-rotor system in the presence of the gro...
In this work, the ground effect phenomena for a rotary wing is investigated both numerically and exp...
In the present work, the aerodynamic performance of the full helicopter PSP in hover flight is inves...