TY  - JOUR
AU  - Zeljković, Vladimir
AU  - Maksimović, Katarina
AU  - Knežević, Jezdimir
PY  - 2010
UR  - https://dais.sanu.ac.rs/123456789/15203
AB  - This paper gives the procedure for the reliability calculation of mechanical components and structures. The stability (buckling) of a tin panel subjected to in-plane combined (normal and shearing) loads is considered in particular. The attention is focused on the buckling analysis of the typical thin-walled aircraft structure such as the skin of wings or fuselage. In this analysis the variables are treated as stochastic: loads, thickness and width of the panel. The numerical example illustrates the procedure. The probability of buckling is calculated for the wing skin of a light trainer aircraft. The effect of the panel thickness (t) and the load factor (j) on the buckling probability is shown. The dimensional tolerance levels affect the critical stress calculation as well as the buckling probability. The variation of the parameters (especially the thickness effect on the buckling) is facilitated by a software program for reliability calculation.
PB  - Beograd : Vojnotehnički institut
T2  - Scientific Technical Review
T1  - Probabilistički proračun gubitka stabilnosti tankih panela pod dejstvom kombinovanog opterećenja
T1  - Probabilistic approach to buckling analysis of thin panels subject to combined loads
SP  - 34
EP  - 38
VL  - 60
IS  - 3-4
UR  - https://hdl.handle.net/21.15107/rcub_dais_15203
ER  - 

@article{
author = "Zeljković, Vladimir and Maksimović, Katarina and Knežević, Jezdimir",
year = "2010",
abstract = "This paper gives the procedure for the reliability calculation of mechanical components and structures. The stability (buckling) of a tin panel subjected to in-plane combined (normal and shearing) loads is considered in particular. The attention is focused on the buckling analysis of the typical thin-walled aircraft structure such as the skin of wings or fuselage. In this analysis the variables are treated as stochastic: loads, thickness and width of the panel. The numerical example illustrates the procedure. The probability of buckling is calculated for the wing skin of a light trainer aircraft. The effect of the panel thickness (t) and the load factor (j) on the buckling probability is shown. The dimensional tolerance levels affect the critical stress calculation as well as the buckling probability. The variation of the parameters (especially the thickness effect on the buckling) is facilitated by a software program for reliability calculation.",
publisher = "Beograd : Vojnotehnički institut",
journal = "Scientific Technical Review",
title = "Probabilistički proračun gubitka stabilnosti tankih panela pod dejstvom kombinovanog opterećenja, Probabilistic approach to buckling analysis of thin panels subject to combined loads",
pages = "34-38",
volume = "60",
number = "3-4",
url = "https://hdl.handle.net/21.15107/rcub_dais_15203"
}

Zeljković, V., Maksimović, K.,& Knežević, J.. (2010). Probabilistički proračun gubitka stabilnosti tankih panela pod dejstvom kombinovanog opterećenja. in Scientific Technical Review
Beograd : Vojnotehnički institut., 60(3-4), 34-38.
https://hdl.handle.net/21.15107/rcub_dais_15203

Zeljković V, Maksimović K, Knežević J. Probabilistički proračun gubitka stabilnosti tankih panela pod dejstvom kombinovanog opterećenja. in Scientific Technical Review. 2010;60(3-4):34-38.
https://hdl.handle.net/21.15107/rcub_dais_15203 .

Zeljković, Vladimir, Maksimović, Katarina, Knežević, Jezdimir, "Probabilistički proračun gubitka stabilnosti tankih panela pod dejstvom kombinovanog opterećenja" in Scientific Technical Review, 60, no. 3-4 (2010):34-38,
https://hdl.handle.net/21.15107/rcub_dais_15203 .