Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Abdelwahid Boutemedjet"'
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::859c0faa89cfa33b083e20a0b0158e7a
https://doi.org/10.1016/j.ast.2018.09.043
https://doi.org/10.1016/j.ast.2018.09.043
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43f64f7cf2e0260647d1cbccd43217c9
https://doi.org/10.1016/j.engfailanal.2018.04.013
https://doi.org/10.1016/j.engfailanal.2018.04.013
Publikováno v:
Measurement. 116:438-450
An experimental investigation was conducted to determine the accuracy of the rolling moment measurement in wind tunnel tests. The test was done in a high Reynolds number blowdown wind tunnel in subsonic, transonic and supersonic speed regimes. The ro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5adae39030e26d3a28d9f52fe7e364eb
https://doi.org/10.1016/j.measurement.2017.11.043
https://doi.org/10.1016/j.measurement.2017.11.043