Add to ORKGThe article presents some peculiarities of lift force calculation method using nonlinear section data. The main task is to determine an influence of iteration procedure on solution accuracy. This evaluation is a part of initiated research on potentials and application limits of the method. Set of accuracy is described in more details. Influence results of iteration procedure are presented for lift calculation of a tapered wing
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX90890 / BLDSC - British Library Do...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
Calculation results for 11 different finite span wings are presented. Calculations were made by a co...
In this article history and development of calculation methods of wing characteristics are presented...
A method is presented for calculating lift distributions for unswept wings with flaps or ailerons us...
A method is presented which allows the use of nonlinear section lift data in the calculation of the ...
The methods of NACA Reports 865 and 1090 have been applied to the calculation of the rolling- and ya...
A method is presented which allows the use of nonlinear section lift data in the calculation of the ...
This paper investigates the importance of nonlinear aeroelastic static analysis in the structural de...
In this paper a computational methodology of aerodynamic interaction between propeller and wing is d...
This master thesis shows, how can be the modified lifting line theory used for preliminary glider de...
A mathematical modeling technique was developed for the lift characteristics of straight wings throu...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...
The joined wing is a new concept of the airplane wing. The forewing and the aft wing are joined toge...
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX90890 / BLDSC - British Library Do...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
Calculation results for 11 different finite span wings are presented. Calculations were made by a co...
In this article history and development of calculation methods of wing characteristics are presented...
A method is presented for calculating lift distributions for unswept wings with flaps or ailerons us...
A method is presented which allows the use of nonlinear section lift data in the calculation of the ...
The methods of NACA Reports 865 and 1090 have been applied to the calculation of the rolling- and ya...
A method is presented which allows the use of nonlinear section lift data in the calculation of the ...
This paper investigates the importance of nonlinear aeroelastic static analysis in the structural de...
In this paper a computational methodology of aerodynamic interaction between propeller and wing is d...
This master thesis shows, how can be the modified lifting line theory used for preliminary glider de...
A mathematical modeling technique was developed for the lift characteristics of straight wings throu...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...
The joined wing is a new concept of the airplane wing. The forewing and the aft wing are joined toge...
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX90890 / BLDSC - British Library Do...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...