12   Artículos

 
en línea
Marin Ivankovic, Milan Vrdoljak, Marijan Andric and Hrvoje Kozmar    
The angle of attack is one of the most important flight parameters. In the framework of the present study, a flight data recording method was designed to analyze the Valasek angle-of-attack estimation method and investigate its applicability for general ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Salvatore Corcione, Vincenzo Cusati, Danilo Ciliberti and Fabrizio Nicolosi    
This paper deals with the estimation of propulsive effects for a three-lifting surface turboprop aircraft concept, with rear engine installation at the horizontal tail tips, conceived to carry up to 130 passengers. This work is focused on how the propuls... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Chawki Abdessemed, Abdessalem Bouferrouk and Yufeng Yao    
This work explores the aerodynamic and aeroacoustic responses of an airfoil fitted with a harmonically morphing Trailing Edge Flap (TEF). An unsteady parametrization method adapted for harmonic morphing is introduced, and then coupled with dynamic meshin... ver más
Revista: Acoustics    Formato: Electrónico

 
en línea
David Communier, Ruxandra Mihaela Botez and Tony Wong    
This paper presents the design and wind tunnel testing of a morphing camber system and an estimation of performances on an unmanned aerial vehicle. The morphing camber system is a combination of two subsystems: the morphing trailing edge and the morphing... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Itzik Klein and Roee Diamant    
Between external position updates, the most useful technique for trajectory estimation of a submerged drifter is dead reckoning (DR). These devices drift with the water current to measure the current?s velocity or to observe physical phenomena. We focus ... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Djahid Gueraiche and Sergey Popov    
In this article, the growth of aerodynamic efficiency and the growth of the wing structural stress is studied for DLR-F4 typical transport aircraft wing-body, after installing classical Whitcomb winglets of different configurations and a delta wingtip fe... ver más
Revista: Aerospace    Formato: Electrónico

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