Add to ORKGThis master thesis shows, how can be the modified lifting line theory used for preliminary glider design an for wing loads determination. It is shown, that relatively accurate results can be obtained at less computational cost in comparison with CFD method
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back w...
Abstract: The preliminary analysis of wing of glider aircraftis presented. It gives a decisive consi...
The aim of the following text is to illustrate a method to predict the aerodynamic impact of a local...
The lifting line theory is widely used for obtaining aerodynamic performance results in various engi...
Lifting-line theory is one simple method of predicting the lift produced by a wing. The traditional ...
Calculation results for 11 different finite span wings are presented. Calculations were made by a co...
In this paper a computational methodology of aerodynamic interaction between propeller and wing is d...
The lifting line theory is widely used for obtaining aerodynamic performance results in various engi...
Conceptual aircraft design uses in most cases either semi-empirical methods or simplified structural...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
The inclusion of static aeroelastic effects is essential to the accurate calculation of the aerodyna...
In this article history and development of calculation methods of wing characteristics are presented...
In this paper a tool, previously developed and validated for the prediction of wing box structural w...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back w...
Abstract: The preliminary analysis of wing of glider aircraftis presented. It gives a decisive consi...
The aim of the following text is to illustrate a method to predict the aerodynamic impact of a local...
The lifting line theory is widely used for obtaining aerodynamic performance results in various engi...
Lifting-line theory is one simple method of predicting the lift produced by a wing. The traditional ...
Calculation results for 11 different finite span wings are presented. Calculations were made by a co...
In this paper a computational methodology of aerodynamic interaction between propeller and wing is d...
The lifting line theory is widely used for obtaining aerodynamic performance results in various engi...
Conceptual aircraft design uses in most cases either semi-empirical methods or simplified structural...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.In t...
A numerical lifting-line method (implemented in an open-source software package) is presented which ...
The inclusion of static aeroelastic effects is essential to the accurate calculation of the aerodyna...
In this article history and development of calculation methods of wing characteristics are presented...
In this paper a tool, previously developed and validated for the prediction of wing box structural w...
A modified lifting line algorithm is considered as a low-cost approach for calculating lift characte...
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back w...
Abstract: The preliminary analysis of wing of glider aircraftis presented. It gives a decisive consi...