• Nenhum resultado encontrado

J. Aerosp. Technol. Manag. vol.3 número3

N/A
N/A
Protected

Academic year: 2018

Share "J. Aerosp. Technol. Manag. vol.3 número3"

Copied!
8
0
0

Texto

Loading

Imagem

Figure 1 depicts the radar signature of a generic glider at  0.5 GHz, for a frontal incidence, taken from the examples  supplied with the CST Microwave Studio ®  (CST, 2010)  package
Figure 2.  The left picture shows that in the MoM all elements are allowed to couple to each other, generating a very dense matrix
Figure 4.  Surface mesh for the object. Zoomed in is a detailed  area near the stabilizers.
Figure 7.  Current distribution caused by a frontal (left) and lateral (right) incidence
+3

Referências

Documentos relacionados

shows the complete model of Sonda III in scale 1:20 installed in the test section of TTP, with one end of the internal balance connected to the model and the other one

The VSB-30 vehicle is a two-stage, unguided, rail launched sounding rocket, consisting of a solid propellant S31 rocket booster, a boost adapter, the second stage S30,

Keywords: Deep space mission, Laser altimeter, Laser rangeinder, ASTER, ALR.. THE FIRST BRAZILIAN MISSION TO DEEP

: hen the reform of incentive instruments of the 1 ational Innovation System took place, more than ten years ago, with the creation of the Sectoral Funds, there were

Abstract: Reinforced thermoplastic structural detail parts and assemblies are being developed to be included in current aeronautic programs. Thermoplastic composite technology

For this, formulations of polyurethane resin loaded with carbon black and NiZn ferrite, with general composition MFe 2 O 4 , where M = Ni, Zn or both elements, homogenized

  Figure 6c shows the normalized  ı az  and  IJ ax  for single lap  bonded  joint  and  all  results  are  again  similar  too.  In  this  case,  it  is  possible 

Reduced assembly time.. assembly tools are required for the bracket installation, which save a lot of assembly time. It is easy to replace the spares by the maintenance staff