Add to ORKGA numerical lifting line method, coupled with a numerical blade element method, is presented as a low computational cost approach to modeling slipstream effects on a finite wing. This method uses a 3D vortex lifting law along with known 2D airfoil data to predict the lift distribution across a wing in the presence of a propeller slipstream. The results are of significant importance in the development of an aerodynamic modeling package for initial stages of vertical take-off and landing (VTOL) aircraft design. An overview of the algorithm is presented, and results compared with published experimental data
Today, wind power is one of the most reliable new energysource serving as an alternative to fossil-f...
An unsteady 3D Panel method has been developed to compute the subsonic aerodynamics of finite thickn...
At present, a number of lifting surface theories exist. By and large most of these theories assume s...
A numerical lifting line method, coupled with a numerical blade element method, is presented as a lo...
A numerical lifting line method, coupled with a numerical blade element method, is presented as a lo...
A combined wing and propeller model is presented as a low-cost approach to first-cut modeling of sli...
A numerical method is presented as a low computational cost approach to modeling an induced propelle...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
In this paper a computational methodology of aerodynamic interaction between propeller and wing is d...
Today, wind power is one of the most reliable new energy source serving as an alternative to fossil-...
In the current work a methodology to quickly estimate propeller slipstream effects on a finite wing,...
In the current work a methodology to quickly estimate propeller slipstream effects on a finite wing,...
A discrete vortex method-based model has been proposed for two-dimensional/three-dimensional ground-...
There is renewed interest into propeller-driven aircraft to improve fuel economy. Some novel concept...
Today, wind power is one of the most reliable new energysource serving as an alternative to fossil-f...
An unsteady 3D Panel method has been developed to compute the subsonic aerodynamics of finite thickn...
At present, a number of lifting surface theories exist. By and large most of these theories assume s...
A numerical lifting line method, coupled with a numerical blade element method, is presented as a lo...
A numerical lifting line method, coupled with a numerical blade element method, is presented as a lo...
A combined wing and propeller model is presented as a low-cost approach to first-cut modeling of sli...
A numerical method is presented as a low computational cost approach to modeling an induced propelle...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
In this paper a computational methodology of aerodynamic interaction between propeller and wing is d...
Today, wind power is one of the most reliable new energy source serving as an alternative to fossil-...
In the current work a methodology to quickly estimate propeller slipstream effects on a finite wing,...
In the current work a methodology to quickly estimate propeller slipstream effects on a finite wing,...
A discrete vortex method-based model has been proposed for two-dimensional/three-dimensional ground-...
There is renewed interest into propeller-driven aircraft to improve fuel economy. Some novel concept...
Today, wind power is one of the most reliable new energysource serving as an alternative to fossil-f...
An unsteady 3D Panel method has been developed to compute the subsonic aerodynamics of finite thickn...
At present, a number of lifting surface theories exist. By and large most of these theories assume s...