Add to ORKGThis paper was published in the Proc. of the SEM XI Annual Conf. on Experimental and Applied Mechanics
This paper presents work performed by the Institute of Aerospace Engineering at the Brno University ...
Abstract: Aiming to realize a low-drag supersonic transport, Busemann biplane concept was adopted in...
In this paper a tool, previously developed and validated for the prediction of wing box structural w...
In tandem airfoil configuration or multiple-lifting-surface layouts, due to the flow interaction amo...
A parametric investigation has been conducted on a new multiple lifting surface configuration. This ...
It is known that in a biplane the load is not distributed equally between the wings. The presence of...
A number of methods have been proposed to estimate the lift of a biplane based mostly on potential f...
The purpose of this investigation was to study the effect of improving the aerodynamic characteristi...
The aerodynamics of flapping wing micro air vehicle (FMAV) is significantly affected by the wing kin...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1926.Includ...
This report deals with the air forces on biplane cellule. The first part of the report deals with th...
The performance of a wing-in-ground effect craft depends mostly on its wing configuration. The aerod...
A parametric investigation has been conducted on a new multiple lifting surface configuration. This ...
[EN] The main objective of this project is to study the aerodynamic interaction between the wings i...
The design of complex aircraft elements such as high-lift devices has large influence on the perform...
This paper presents work performed by the Institute of Aerospace Engineering at the Brno University ...
Abstract: Aiming to realize a low-drag supersonic transport, Busemann biplane concept was adopted in...
In this paper a tool, previously developed and validated for the prediction of wing box structural w...
In tandem airfoil configuration or multiple-lifting-surface layouts, due to the flow interaction amo...
A parametric investigation has been conducted on a new multiple lifting surface configuration. This ...
It is known that in a biplane the load is not distributed equally between the wings. The presence of...
A number of methods have been proposed to estimate the lift of a biplane based mostly on potential f...
The purpose of this investigation was to study the effect of improving the aerodynamic characteristi...
The aerodynamics of flapping wing micro air vehicle (FMAV) is significantly affected by the wing kin...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1926.Includ...
This report deals with the air forces on biplane cellule. The first part of the report deals with th...
The performance of a wing-in-ground effect craft depends mostly on its wing configuration. The aerod...
A parametric investigation has been conducted on a new multiple lifting surface configuration. This ...
[EN] The main objective of this project is to study the aerodynamic interaction between the wings i...
The design of complex aircraft elements such as high-lift devices has large influence on the perform...
This paper presents work performed by the Institute of Aerospace Engineering at the Brno University ...
Abstract: Aiming to realize a low-drag supersonic transport, Busemann biplane concept was adopted in...
In this paper a tool, previously developed and validated for the prediction of wing box structural w...