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

While previous studies have focused on gain and directivity enhancement of wire-medium antennas (Hrabar et al. 2013), here we present a conceptual study of a wire

In addition, this radar cross section model can be directly applied to the radar detection process to calculate the detection probability of a speciic aircraft at any attitude..

(2010) have estimated aircraft stability derivatives from acquired flight data using the Output Error Method (OEM) technique; in this study, longitudinal and lateral dynamics

In this study, the physics behind the wake structure, the transition from one low regime to another and the thrust/lit performance of a sinusoidally lapping symmetric airfoil over

Atmospheric multiphase low for an aircrat icing can be treated as a compressible and dilute multiphase low ignoring the droplet efects in air lows since the mass loading ratio of the

During the NNEB rainy season, a southward GRAD — due to positive SSTAs in the tropical South Atlantic and/or negative in the tropical North Atlantic — would be related to

ABSTRACT: This paper brings the irst results concerning a new analytic model to evaluate atmospheric dispersion in rocket launch scenarios, namely Generalized Integral

Figure 4.30 - Position and trajectory rotations fault tolerant control to motor 1 failure, safe landing.. The black line represents the setpoint and the blue line the