Zobrazeno 1 - 10
of 38
pro vyhledávání: '"Isaković Jovan"'
Publikováno v:
Scientific Technical Review, Vol 66, Iss 4, Pp 34-39 (2016)
As a part of a periodic health monitoring of the wind tunnel structure, instrumentation and flow quality, a series of tests of an AGARD-C calibration model was performed in the 1.5 m T-38 trisonic wind tunnel of the Military Technical Institute (VTI)
Externí odkaz:
https://doaj.org/article/83b1438511bb499788b7037784f53b04
Publikováno v:
FME Transactions, Vol 44, Iss 1, Pp 1-9 (2016)
The flow parameters control in wind tunnels is an area of intense research in recent years, with the aim of improving quality and efficiency of the wind tunnel operation. In this paper, an attempt is made to contribute to a better understanding of th
Externí odkaz:
https://doaj.org/article/a03abf30364d4a9d9942fb26aabe640d
Publikováno v:
Scientific Technical Review, Vol 64, Iss 3, Pp 40-46 (2014)
The external six-component wind tunnel balance designed and manufactured in the Military Technical Institute is described in this paper. The balance is of a platform type. Aerodynamic load which acts on a model in the wind tunnel test section is tran
Externí odkaz:
https://doaj.org/article/0746d87a201c403d9dfaa37d357c7a6d
Publikováno v:
FME Transactions, Vol 42, Iss 3, Pp 212-218 (2014)
A necessity to test a standard model testing for establishing confidence in the wind-tunnel flow quality and the validity of the test-data has been recognized in the Experimental Aerodynamics Laboratory of the Military Technical Institute (VTI) in Be
Externí odkaz:
https://doaj.org/article/04118d38ddd746f6882ee6993c33b01f
Publikováno v:
FME Transactions, Vol 41, Iss 1, Pp 33-40 (2013)
The paper presents the challenge of finding the best criterion in selecting adequate control algorithm for electro-hydraulic actuator with a defined load. The ideal control algorithm that adapts to the actual configuration of electro-hydraulic actuat
Externí odkaz:
https://doaj.org/article/8788d1cb270d42788aabf41b89e1caa9
Publikováno v:
FME Transactions, Vol 41, Iss 3, Pp 189-194 (2013)
Measurement of the direct damping derivative in roll in the T-38 wind tunnel is described in this paper. The T-38 wind tunnel data for the Basic Finner Model and Modified Basic Finner model are shown. The forced oscillation technique was used for the
Externí odkaz:
https://doaj.org/article/c9c391352e0549fa9c239d416df944f3
Publikováno v:
FME Transactions, Vol 41, Iss 2, Pp 114-119 (2013)
One of the most difficult aspects of aircraft and missile development is defining stability and control characteristics. The best way to obtain model-scale dynamic stability derivatives is to perform experiments in wind tunnels having high Reynolds n
Externí odkaz:
https://doaj.org/article/95dc6e25fbe44f56b835a61d27ce57fd
Autor:
Damljanović, Dijana, Vuković, Djordje, Ilić, Biljana, Ocokoljić, Goran, Isaković, Jovan, Miloš, Marko
Publikováno v:
In Materials Today: Proceedings 2023 93 Part 4:712-718
Publikováno v:
In Materials Today: Proceedings 2019 12 Part 2:239-245
Publikováno v:
In Materials Today: Proceedings 2018 5(13) Part 2:26476-26481