Zobrazeno 1 - 10
of 29
pro vyhledávání: '"Dijana Damljanović"'
Publikováno v:
Advances in Mechanical Engineering, Vol 14 (2022)
Higher than anticipated supersonic starting loads in the VTI T-38 wind tunnel were a consequence of higher than designed minimum start pressures. Initially, high starting loads limited the usefulness of the facility at high supersonic Mach numbers. O
Externí odkaz:
https://doaj.org/article/5689d4dc868d4494a7e7e96544f1e97b
Publikováno v:
Aerospace, Vol 8, Iss 10, p 275 (2021)
Published results for standard wind tunnel models at non-standard test conditions are quite rare and/or may not be available. It has been found that those results are a useful aid in preparations for a number of wind tunnel tests in the Military Tech
Externí odkaz:
https://doaj.org/article/23a8cd1ae8014e8cb4c36c24b7f6b311
Autor:
Dijana Damljanović, Aleksandar Vitić
Publikováno v:
Vojnotehnički Glasnik, Vol 55, Iss 4, Pp 389-399 (2007)
U radu su prikazani rezultati eksperimentalnih ispitivanja rolerona postojećeg projektila u aerotunelu T-38 Vojnotehničkog instituta. Za smanjenje ugaone brzine valjanja koriste se roleroni kao najjednostavniji uređaji. Oni predstavljaju žiroskop
Externí odkaz:
https://doaj.org/article/e23793a725704c7086fb25c639faf782
Autor:
Dijana Damljanović, Slavica Ristić
Publikováno v:
Vojnotehnički Glasnik, Vol 53, Iss 5, Pp 406-417 (2005)
U radu su prikazani rezultati merenja aerodinamičkih sila i momenata, kao i vizualizacija strujanja u graničnom sloju na krilima i krmilima modela laserski vođene bombe. Ispitivanje je izvršeno u aerotunelu T-38. Analiziranje uticaj rastojanja vr
Externí odkaz:
https://doaj.org/article/a13f37fcf2104e10a0d7c6296af026f2
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 235:1129-1145
The goal of this work is to build a unique numerical method to obtain the basic aerodynamic characteristics of the aircraft and to enable a wide application of the method in the analysis of some aerodynamic characteristics of the aircraft, without us
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e5f526e4171292d24b5311fecc135a85
https://doi.org/10.1177/0954410020966859
https://doi.org/10.1177/0954410020966859
Publikováno v:
FME Transactions. 48:770-778
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://explore.openaire.eu/search/publication?articleId=doi_________::2441a0fd78524eb8ac000ef97d46f286
https://doi.org/10.5937/fme2004770o
https://doi.org/10.5937/fme2004770o
Publikováno v:
FME Transactions. 48:761-769
AGARD-B is a widely-used configuration of a standard wind tunnel model. Beside its originally intended application for correlation of data from supersonic wind tunnel facilities, it was tested in a wide range of Mach numbers and, more recently, used
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7ee640d77056b93e50a6f1c0533ba4ac
https://doi.org/10.5937/fme2004761d
https://doi.org/10.5937/fme2004761d
Autor:
Dijana Damljanović, Djordje Vukovic
Publikováno v:
Chinese Journal of Aeronautics, Vol 32, Iss 7, Pp 1565-1576 (2019)
Responding to a need for experimental data on a standard wind tunnel model at high angles of attack in the supersonic speed range, and in the absence of suitable reference data, a series of tests of two HB-2 standard models of different sizes was per
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::40f7ac141f94574746e301745e039082
https://doi.org/10.1016/j.cja.2019.03.022
https://doi.org/10.1016/j.cja.2019.03.022
Publikováno v:
Scopus-Elsevier
An increased number of requirements for supersonic wind tunnel tests at high angles of attack (AoA) opened the problem of the validation of a high-AoA wind tunnel setup in the Experimental Aerodynamics Laboratory of VTI (Military Technical Institute)
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b991fb15bbfdfa0288a77a49d33ece3b
https://doi.org/10.1016/j.matpr.2019.03.120
https://doi.org/10.1016/j.matpr.2019.03.120
Publikováno v:
Scientific Technical Review (2021) 71(2):19-25
Experimental verification of base-bleed effects on aerodynamic characteristics for the supersonic flight stages was requested during the development of an axi-symmetric projectile. The experimental setup for testing base-bleed configurations of the p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::17fc707df0dc30b58d429f2def85d292
http://scindeks.ceon.rs/article.aspx?artid=1820-02062102019D
http://scindeks.ceon.rs/article.aspx?artid=1820-02062102019D