Výsledky vyhledávání - "Dodić Marjan"

Akademický článek

Numerička analiza dinamičkog ponašanja kompozitnog saćastog panela ispunjenog cevčicama pod dejstvom udarnog opterećenja male brzine u ravni panela

Autor: Djemaoune Younes A., Krstić Branimir B., Rašuo Boško P., Rašić Stefan P., Radulović Daniel R., Dodić Marjan D.

Publikováno v: FME Transactions, Vol 49, Iss 4, Pp 969-976 (2021)

Honeycomb sandwich structures, composed of many regularly arranged hexagonal cores and two skins, show excellent impact performance due to strong energy absorption capability under impact loads. In this paper, a numerical study of low velocity impact

Externí odkaz: https://doaj.org/article/78c0abe595154f259ae2100c039d8bd5

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Akademický článek

Numerical investigation of open-hole damaged Nomex™ honeycomb panel under three-point bending load

Autor: Djemaoune Younes, Krstić Branimir, Radulović Daniel, Rašić Stefan, Dodić Marjan

Publikováno v: Scientific Technical Review, Vol 71, Iss 2, Pp 14-18 (2021)

In the present study, a numerical investigation of three-point bending test of the open-hole damaged sandwich structures with Nomex TM honeycomb core and aluminium alloy skins is carried out. In order to evaluate the degradation of the mechanical pro

Externí odkaz: https://doaj.org/article/fd2454c0c8324949b3ab684fb4db255c

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Akademický článek

Single rotor helicopter parasite drag estimation in the preliminary design stage

Autor: Dodić Marjan D., Krstić Branimir B., Rašuo Boško P.

Publikováno v: Tehnika, Vol 73, Iss 1, Pp 65-77 (2018)

This paper presents the methodology for the rapid estimation of the single rotor helicopter parasite drag in the forward flight in the preliminary design phase. The aerodynamic drag of fuselage, main rotor hub, landing gear and the other, non-rotatin

Externí odkaz: https://doaj.org/article/d2b2f2a308074614a38630eae78e548c

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Akademický článek

On the effective shear modulus of composite honeycomb sandwich panels

Autor: Rebhi Lamine, Dinulović Mirko, Andrić Predrag, Dodić Marjan, Krstić Branimir

Publikováno v: Scientific Technical Review, Vol 66, Iss 4, Pp 59-65 (2016)

In the presented paper the effective shear modulus of composite plates with honeycomb core is determined. This elastic coefficient represents one very important property, especially in constructions subjected to torsion and combined bending - torsion

Externí odkaz: https://doaj.org/article/fb0b319b5641494ca8efb6a5ef2a29bc

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