Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Marija Samardžić"'
Autor:
Jasminka Talapko, Erwin Frauenheim, Martina Juzbašić, Matej Tomas, Suzana Matić, Melita Jukić, Marija Samardžić, Ivana Škrlec
Publikováno v:
Microorganisms, Vol 10, Iss 2, p 255 (2022)
Legionella pneumophila is defined as a bacterium that can cause severe pneumonia. It is found in the natural environment and in water, and is often found in water tanks. It can be an integral part of biofilms in nature, and the protozoa in which it c
Externí odkaz:
https://doaj.org/article/5dfc41de1652463aac3f83b902641028
Autor:
Aleksandar Vitić, Marija Samardžić
Publikováno v:
Vojnotehnički Glasnik, Vol 56, Iss 3, Pp 16-27 (2008)
Pri ispitivanju modela u "rafalnom" aerotunelu sa prekidnim dejstvom T-38, na Mahovim brojevima većim od 2, moraju se uzeti u obzir prelazne pojave koje se javljaju na početku i na kraju rada aerotunela. To su stanja kada su model i aerovaga izlož
Externí odkaz:
https://doaj.org/article/13f8ff2703514f1d9b703fd3817ee18d
Publikováno v:
Scientific Technical Review. 69:36-42
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ab793e8037aed8a78febf806439cd6b
https://doi.org/10.5937/str1902036s
https://doi.org/10.5937/str1902036s
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
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
Publikováno v:
Scientific Technical Review. 68:31-36
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9279f92e8ec0adddfdadd1355a302fe6
https://doi.org/10.5937/str1803031s
https://doi.org/10.5937/str1803031s
Autor:
Vanja Stefanović-Gobeljić, Miodrag Milenković-Babić, Marija Samardžić, Vuk Antonić, Milica Marjanović
Publikováno v:
Aircraft Engineering and Aerospace Technology. 89:911-919
Purpose This paper presents the longitudinal stability analysis of a single tractor propeller airplane LASTA at high engine power settings. This analysis is part of the ongoing process of certifying the airplane for civil use according to the civil r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6495afac468565f3b62b7082c1147a3
https://doi.org/10.1108/aeat-02-2016-0026
https://doi.org/10.1108/aeat-02-2016-0026
Autor:
Marija Samardžić, Dušan Ćurčić, Stevan Maksimović, Boško Rašuo, Nenad Vidanović, Gordana Kastratović
Publikováno v:
Aerospace Science and Technology. 65:26-45
The aim of the paper is to establish and demonstrate the significant capacity and performances of a well predictive numerical environment, developed for multidisciplinary design optimization (MDO) purposes, which presents one more contribution in cas
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::37c4fcf76baf2f5ab366996106844183
https://doi.org/10.1016/j.ast.2017.02.010
https://doi.org/10.1016/j.ast.2017.02.010
Publikováno v:
Journal of Spacecraft and Rockets. 54:672-682
The roll damping dynamic stability derivative for a modified basic finner missile at transonic and supersonic speeds is calculated using quasi-stationary and unsteady computational fluid dynamics m...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29c2c72b2b7a0e27c68db37266af88f4
https://doi.org/10.2514/1.a33674
https://doi.org/10.2514/1.a33674
Publikováno v:
Aerospace Science and Technology. 50:272-280
In this paper an elastic element of the forced oscillation apparatus for dynamic measurements in the T-38 wind tunnel is described. The forced oscillation apparatus consists of the elastic element, dynamic balance, actuator arm, hydraulic driving mec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eff4408b2c228f874d6ef7c5d2d2b10e
https://doi.org/10.1016/j.ast.2016.01.011
https://doi.org/10.1016/j.ast.2016.01.011