Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Lamine Rebhi"'
Publikováno v:
Aerospace Science and Technology. 84:464-483
In this paper, the aerodynamic design procedure of a mini unmanned aerial vehicle, intended to perform aerial reconnaissance at low altitude and low Reynolds number, was summarized. Design process was divided into two major parts: conceptual design p
Autor:
Lamine Rebhi, Nikola Vučetić, Branimir Krstic, Miroslav Milutinović, Narimane Rezgui, Abdelwahid Boutemedjet, Ljubica Totovski
Publikováno v:
Engineering Failure Analysis. 90:476-488
The antenna of military aircraft was fractured into two pieces during the flight mission. The fracture occurred in bottom part of antenna. The lower portion of the antenna stayed attached to the fuselage, whereas the upper portion fall off the aircra
Publikováno v:
FME Transaction. 45:537-542
Autor:
Predrag Andric, Lamine Rebhi, Mirko Dinulović, Marjan Dodic, Nada Ilic, Dragan Trifkovic, Branimir Krstic
Publikováno v:
Engineering Failure Analysis. 70:351-363
The mounting bolt of helicopter main gearbox support strut was fractured into two pieces during the flight mission. The fracture occurred at the root of the first engaged thread of the bolt-nut assembly. Visual inspection of the fracture zone reveale
Autor:
Lamine Rebhi, Marjan Dodic, Milorad Milovančević, Nabil Khettou, Branimir Krstic, Sreten Peric, Dragan Trifkovic
Publikováno v:
Engineering Failure Analysis. 63:121-130
The skid landing gear of a military helicopter failed while the helicopter was moored on the ground at the airport. The rear cross tube of the landing gear assembly was found fractured into two separated pieces. The fracture occurred in the right fla
Publikováno v:
Scientific Technical Review. 66:59-65