In this presentation, we will concentrate on typical Ground Static Test (GST) and Finite Element (FE) software comparisons. It is necessary to note, that standard GST are obligatory for any new aircraft configuration. We can mention here the investigations of the AeroTAXITM, a small aircraft configuration, using PRODERA® equipment. A Finite Element Model (FEM) of the AeroTAXITM has been developed in PATRAN/NASTRAN®, partly from a previous ANSYS® model. FEM can be used to investigate potential structural modifications or changes with realistic component corrections. Model validation should be part of every modern engineering analysis and quality assurance procedure
The new trainer aircraft PC-21 is presently under development by the Swiss company Pilatus Aircraft ...
This paper has been funded by the internal resources of Structural Analyses Department, VZLU Pragu...
Small modeling errors in the finite element model will eventually induce errors in the structural fl...
The paper discusses possibilities to make use of the finite element model (FE model) to prepare and ...
The paper discusses possibilities to make use of the finite element model (FE model) to prepare and ...
The paper discusses possibilities to make use of the finite element model (FE model) to prepare and ...
In this presentation, we will concentrate on typical Ground Vibration Test (GVT) and FiniteElement (...
The design of airplane, when plane is in the flight mode it is because of wings on both sides. While...
The aeroelastic stability certification of today's civil aircraft structures requires validated anal...
Within the framework of the Flexible Aircraft WP 2500 program a research ground vibration test on th...
Airplanes are designed to stay aloft with the help of wings on both sides. In operation at cruising ...
The article presents the results obtained within a study on the effective validation of aeronautical...
This project details the structural analysis of the wings of two Radio-controlled aircraft, designed...
Modal parameters such as eigenfrequencies, damping ratios, and mode shapes of aircraft prototypes ar...
The finite element model is the main tool used by helicopter manufacturers for the analysis of helic...
The new trainer aircraft PC-21 is presently under development by the Swiss company Pilatus Aircraft ...
This paper has been funded by the internal resources of Structural Analyses Department, VZLU Pragu...
Small modeling errors in the finite element model will eventually induce errors in the structural fl...
The paper discusses possibilities to make use of the finite element model (FE model) to prepare and ...
The paper discusses possibilities to make use of the finite element model (FE model) to prepare and ...
The paper discusses possibilities to make use of the finite element model (FE model) to prepare and ...
In this presentation, we will concentrate on typical Ground Vibration Test (GVT) and FiniteElement (...
The design of airplane, when plane is in the flight mode it is because of wings on both sides. While...
The aeroelastic stability certification of today's civil aircraft structures requires validated anal...
Within the framework of the Flexible Aircraft WP 2500 program a research ground vibration test on th...
Airplanes are designed to stay aloft with the help of wings on both sides. In operation at cruising ...
The article presents the results obtained within a study on the effective validation of aeronautical...
This project details the structural analysis of the wings of two Radio-controlled aircraft, designed...
Modal parameters such as eigenfrequencies, damping ratios, and mode shapes of aircraft prototypes ar...
The finite element model is the main tool used by helicopter manufacturers for the analysis of helic...
The new trainer aircraft PC-21 is presently under development by the Swiss company Pilatus Aircraft ...
This paper has been funded by the internal resources of Structural Analyses Department, VZLU Pragu...
Small modeling errors in the finite element model will eventually induce errors in the structural fl...