This paper deals with structural static or stability analysis of straight beams, when the bending-torsion coupling is considered. A practical case is the lateral buckling analysis of high cross-section beams which involv...
The trailing edge region of a single element wing fitted with Gurney flap at low Reynolds numbers has been studied.
The complex flow separation phenomena on airfoils with Gurney flap at low Reynolds numbers have some sp...
The development of the world economy and the globally accelerated diversification of production led to the need of widening the economic cooperation. The need of cooperation increased in various sectors of the global eco...
A supplying system for air with precisely controlled temperature, pressure, flow and speed has been designed in order to test the flueric actuator. All these parameters are monitored and the acquired data are stored on a...
The main objective of this paper is to develop a set of tools and integrate techniques in a software package dedicated to stress analysis of aeronautical structures.
Integral Method for Structural Analysis of Beams with Bending-Torsion Coupling
This paper deals with structural static or stability analysis of straight beams, when the bending-torsion coupling is considered. A practical case is the lateral buckling analysis of high cross-section beams which involv...
[b]Analysis of low Reynolds number flow past Gurney flap[/b]
The trailing edge region of a single element wing fitted with Gurney flap at low Reynolds numbers has been studied. The complex flow separation phenomena on airfoils with Gurney flap at low Reynolds numbers have some sp...
Cooperation Forms in the Aeronautics Industry
The development of the world economy and the globally accelerated diversification of production led to the need of widening the economic cooperation. The need of cooperation increased in various sectors of the global eco...
Optimization of the flueric actuators testing system
A supplying system for air with precisely controlled temperature, pressure, flow and speed has been designed in order to test the flueric actuator. All these parameters are monitored and the acquired data are stored on a...
[b]INPROV - an environment for stress analysis of aeronautical structures[/b]
The main objective of this paper is to develop a set of tools and integrate techniques in a software package dedicated to stress analysis of aeronautical structures.