• Nenhum resultado encontrado

Lat. Am. j. solids struct. vol.13 número12

N/A
N/A
Protected

Academic year: 2018

Share "Lat. Am. j. solids struct. vol.13 número12"

Copied!
18
0
0

Texto

Loading

Imagem

Figure 2 : Aircraft platform, elevators and ailerons used as load alleviators.
Figure 4: Feedback Control System architecture.
Figure 5: Vertical Load Factor, Comparison between Elastic and Rigid aircraft.
Figure 6: Control Surface deflections, Comparison between Elastic and Rigid aircraft.
+4

Referências

Documentos relacionados

The comparison of finite element analysis results match with the test results available in the literature shows that the analysis model can simulate the buckling behaviour

This paper dealt with free vibration analysis of thick double curved composite sandwich panels with simply supported or fully clamped boundary conditions based on a new

[r]

An investigation on the effect of uniform tensile in plane force on the radially symmetric vibratory characteristics of functionally graded circular plates of linearly

From these figures, it is clear that as the clay content is increased, there is increase in damping factor which is due to the presence of the additional medium (clay) in

[r]

The implementation of this signal processing algorithm in the damage detection method permits the identification of small frequency changes, and consequently

[r]