Zobrazeno 1 - 10
of 42
pro vyhledávání: '"Živković SA"'
Autor:
Radenković Marina, Momčilović Miloš, Petrović Jelena, Mraković Ana, Relić Dubravka, Popović Aleksandar, Živković Sanja
Publikováno v:
Journal of the Serbian Chemical Society, Vol 87, Iss 7-8, Pp 939-952 (2022)
Presented research aimed to develop an alternative approach for the estimation of biosorption capability of sunflower husk. The acid-pretreated sunflower biomass was characterized by scanning electron microscopy combined with energy dispersive X-Ray
Externí odkaz:
https://doaj.org/article/c50dcb49df10408da8146ef6683aa6e2
Autor:
Đokić Dragoslav, Terzić Dragan, Rajičić Vera, Živković Sanja, Oro Violeta, Milenković Jasmina, Koprivica Ranko
Publikováno v:
Journal on Processing and Energy in Agriculture, Vol 25, Iss 1, Pp 32-35 (2021)
The paper presents the results of the cleaning process of five different lots of natural alfalfa seeds and five different lots of natural red clover seeds. Natural alfalfa and red clover seeds had 75 % to 77 % purity. The experiment was performed in
Externí odkaz:
https://doaj.org/article/75f6ef1d40794273a135bc34f82e0bc4
Autor:
Marković Jordan, Anđelković Snežana, Zornić Vladimir, Kostić Ivica, Blagojević Milomir, Vasić Tanja, Živković Sanja
Publikováno v:
Biotechnology in Animal Husbandry, Vol 36, Iss 4, Pp 477-485 (2020)
Cell wall content generally is regarded as the most important factor affecting forage utilization because it comprises the major fraction of forage dry matter and is correlated with forage intake and digestibility. The experiment was carried out to e
Externí odkaz:
https://doaj.org/article/42daef5221464c55abbdd3b29bfc89cf
Publikováno v:
FME Transactions, Vol 48, Iss 4, Pp 770-778 (2020)
The flow field phenomena that occur as a result of thrust vector control (TVC) system activity on a missile with lateral jets are very complex and influence all other components of the missile. Influence is more significant when TVC is generating com
Externí odkaz:
https://doaj.org/article/2623c50b976f4957b50880d708a74576
Autor:
Gligorijević Nikola, Rodić Vesna, Pavković Bojan, Bogdanov Jovica, Živković Saša, Bajić Zoran
Publikováno v:
Scientific Technical Review, Vol 69, Iss 2, Pp 8-16 (2019)
Rocket motor propellant grain, cast or bonded into the motor chamber or solid coating, is exposed to various loads during its service life. Rocket propellant is a viscoelastic material, whose mechanical properties strongly depend on temperature and s
Externí odkaz:
https://doaj.org/article/6177bafe475f46bb8a9c786115248f9a
Publikováno v:
Srpski Arhiv za Celokupno Lekarstvo, Vol 146, Iss 7-8, Pp 378-383 (2018)
Introduction/Objective. Maxillary or mandibular retrognathism are common dentofacial deformities treated by combined orthodontic-surgical treatment. Surgical maxillary or mandibular advancement changes the position and strain of surrounding structure
Externí odkaz:
https://doaj.org/article/39f0821af7cb44b9a8f9dda2bd182511
Publikováno v:
Scientific Technical Review, Vol 68, Iss 2, Pp 11-16 (2018)
Dispersion of the impact points of the unguided rockets is a consequence of disturbances, such as thrust misalignments, rocket asymmetry, manufactoring inacuracy, etc. Influence of some disturbances are most significant in the initial phase of flight
Externí odkaz:
https://doaj.org/article/0bb5d72f766747a9a0f9d72a2727485b
Autor:
Gligorijević Nikola, Nešić Jovica, Bogdanov Jovica, Pavković Bojan, Živković Saša, Tanaskovski Bojan
Publikováno v:
Scientific Technical Review, Vol 68, Iss 1, Pp 33-39 (2018)
The paper discusses the influence of ignition mixture granulation onto the regime of rocket motor ignition. Igniter tests were performed in manometric bomb and pressure distribution was measured. In each test different granulations of the same mixtur
Externí odkaz:
https://doaj.org/article/1b446fc1ed914678a39c7429cced9534
Autor:
Marjanović Goran, Kozomara Stevan, Stojković Srđan, Gligorijević Nikola, Živković Saša, Pavković Bojan
Publikováno v:
Scientific Technical Review, Vol 68, Iss 3, Pp 56-63 (2018)
The main propulsive group of anti-armor guided missile is reinforced by additional propulsive group with the aim to increase the range. Final concept of the propulsion has been adopted after consideration of several proposed solutions. Two additional
Externí odkaz:
https://doaj.org/article/2f578b78bbb5492984d88be0f3f4ae3f
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