| dc.contributor.author | Žiliukas, Antanas | |
| dc.date.accessioned | 2023-09-18T17:48:24Z | |
| dc.date.available | 2023-09-18T17:48:24Z | |
| dc.date.issued | 2010 | |
| dc.identifier.issn | 1648-7788 | |
| dc.identifier.other | (BIS)VGT02-000021304 | |
| dc.identifier.uri | https://etalpykla.vilniustech.lt/handle/123456789/126343 | |
| dc.description.abstract | Laminated constructional elements have widespread applications in aerospace. This paper presents of the buckling for E-Glass. Design solution based by the criteria of strength materials. The delamination of composite constructional elements is determined by the normal and shear stress. The non-linear strength criterion suggested by the author in case of complex state of stress. | eng |
| dc.description.abstract | Kompozitinių konstrukcijų elementų atsisluoksniavimas nustatomas remiantis normaliniais ir tangentiniais įtempiais. Autorius siūlo netiesinį stiprumo kriterijų, įvertinantį sudė tingą įtempių būvį sprendžiant kompozitų atsisluoksniavimo problemą. | lit |
| dc.format | PDF | |
| dc.format.extent | p. 38-42 | |
| dc.format.medium | tekstas / txt | |
| dc.language.iso | eng | |
| dc.relation.isreferencedby | Academic Search Complete | |
| dc.relation.isreferencedby | Central & Eastern European Academic Source (CEEAS) | |
| dc.relation.isreferencedby | Scopus | |
| dc.source.uri | http://www.tandfonline.com/doi/pdf/10.3846/aviation.2010.06 | |
| dc.title | Delamination during buckling of composite constructional elements | |
| dc.type | Straipsnis Scopus DB / Article in Scopus DB | |
| dcterms.references | 17 | |
| dc.type.pubtype | S2 - Straipsnis Scopus DB / Scopus DB article | |
| dc.contributor.institution | Vilniaus Gedimino technikos universitetas | |
| dc.contributor.faculty | Antano Gustaičio aviacijos institutas / Antanas Gustaitis Aviation Institute | |
| dc.subject.researchfield | T 009 - Mechanikos inžinerija / Mechanical enginering | |
| dc.subject.lt | Atsisluoksniavimas | |
| dc.subject.lt | Kompozitas | |
| dc.subject.lt | Stiprumo kriterijus | |
| dc.subject.en | Delamination | |
| dc.subject.en | Composite | |
| dc.subject.en | Strength criterion | |
| dcterms.sourcetitle | Aviation | |
| dc.description.issue | no. 2 | |
| dc.description.volume | Vol. 14 | |
| dc.publisher.name | Technika | |
| dc.publisher.city | Vilnius | |
| dc.identifier.doi | 2-s2.0-77954907440 | |
| dc.identifier.doi | 10.3846/aviation.2010.06 | |
| dc.identifier.elaba | 3911756 | |
