Building on the well-known Prandtl lifting line, this work proposes an extended framework for mollified lifting lines, which is valid for multidimensional Gaussian smoothings. The smoothing length scale σ can be taken as constant or variable across the span. In this framework, slender lifting device and its wake are represented by a mollified vortex tube and a mollified vortex sheet. Although the resulting formulation is similar to the original one, it is shown that a sectional mean downwash must be used in the integrodifferential equation from which the circulation distribution is obtained. Interestingly, it is also shown that this equation is unaffected by the presence of mollification in the streamwise direction. As an application, the c...
The numerical study of the wake of full-scale slender devices such as aircraft wings and wind turbin...
Lifting-line theory is one simple method of predicting the lift produced by a wing. The traditional ...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
An unsteady linear lifting line method for the determination of the circulation and lift distributio...
An unsteady linear lifting line method for the determination of the circulation and lift distributio...
A closed-form solution for the downwash in the plane of symmetry of an elliptically loaded line is g...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
The problem of a wing placed in a flow that is nonuniform in the spanwise direction is of interest t...
The lifting line theory is widely used for obtaining aerodynamic performance results in various engi...
The perturbation field induced by a line vortex in a supersonic stream and the downwash behind a sup...
Many adaptations of the Lifting-Line Theory have been developed since its conception to aid in preli...
The lifting line theory is widely used for obtaining aerodynamic performance results in various engi...
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
Lift–dominated pointed aircraft configurations are considered in the transonic range. To make the ap...
At present, a number of theories exist for the calculation of lift on delta wings with leading edge ...
The numerical study of the wake of full-scale slender devices such as aircraft wings and wind turbin...
Lifting-line theory is one simple method of predicting the lift produced by a wing. The traditional ...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
An unsteady linear lifting line method for the determination of the circulation and lift distributio...
An unsteady linear lifting line method for the determination of the circulation and lift distributio...
A closed-form solution for the downwash in the plane of symmetry of an elliptically loaded line is g...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
The problem of a wing placed in a flow that is nonuniform in the spanwise direction is of interest t...
The lifting line theory is widely used for obtaining aerodynamic performance results in various engi...
The perturbation field induced by a line vortex in a supersonic stream and the downwash behind a sup...
Many adaptations of the Lifting-Line Theory have been developed since its conception to aid in preli...
The lifting line theory is widely used for obtaining aerodynamic performance results in various engi...
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
Lift–dominated pointed aircraft configurations are considered in the transonic range. To make the ap...
At present, a number of theories exist for the calculation of lift on delta wings with leading edge ...
The numerical study of the wake of full-scale slender devices such as aircraft wings and wind turbin...
Lifting-line theory is one simple method of predicting the lift produced by a wing. The traditional ...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...