Add to ORKGUsing the Gauss-type quadrature formulas one discretizes the hyper singular integral equations of the lifting line with ground or tunnel effects. Numerical calculations are performed for the elliptical and rectangular flat wings. Ground and tunnel effects are pointed out. Key words: lifting line; hyper singular integral equation; discretization; ground and tunnel effects. 1
This thesis presents a new method of solution for incompressible flow analysis past airfoils in the ...
AbstractMulthopp's subsonic lifting surface theory includes the calculation of a singular double int...
This article is intended as a contribution to the theory of the lifting surface. The aerodynamics of...
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...
The present work offers a simplification in the solution of Prandtl's lifting line equation. The equ...
The solution of the lifting line equation Prandtl in wing theory is viewed afresh. Some new aspects ...
The paper refers to the solution of the integral equation for the acceleration (or pressure) potenti...
Bibliography: leaves 164-172.xii, 172 leaves : ill. (some col.) ; 30 cm.The task of calculating the ...
A surface integral is developed which yields solutions of the linearized partial differential equati...
Building on the well-known Prandtl lifting line, this work proposes an extended framework for mollif...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
A computer program 'called LAWS has been developed for the Lift Analysis of Wings In Supersonic flow...
A method utilizing source singularities is presented for obtaining the linearized downwash field due...
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
This thesis presents a new method of solution for incompressible flow analysis past airfoils in the ...
AbstractMulthopp's subsonic lifting surface theory includes the calculation of a singular double int...
This article is intended as a contribution to the theory of the lifting surface. The aerodynamics of...
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...
The present work offers a simplification in the solution of Prandtl's lifting line equation. The equ...
The solution of the lifting line equation Prandtl in wing theory is viewed afresh. Some new aspects ...
The paper refers to the solution of the integral equation for the acceleration (or pressure) potenti...
Bibliography: leaves 164-172.xii, 172 leaves : ill. (some col.) ; 30 cm.The task of calculating the ...
A surface integral is developed which yields solutions of the linearized partial differential equati...
Building on the well-known Prandtl lifting line, this work proposes an extended framework for mollif...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
A computer program 'called LAWS has been developed for the Lift Analysis of Wings In Supersonic flow...
A method utilizing source singularities is presented for obtaining the linearized downwash field due...
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
This thesis presents a new method of solution for incompressible flow analysis past airfoils in the ...
AbstractMulthopp's subsonic lifting surface theory includes the calculation of a singular double int...
This article is intended as a contribution to the theory of the lifting surface. The aerodynamics of...