- Tytuł:
- Post-critical deformation of thin-walled load-bearing aircraft structure representing fragment of the one-way torsion box
- Autorzy:
-
Kopecki, Tomasz
Lis, Tomasz
Mazurek, Przemysław - Powiązania:
- https://bibliotekanauki.pl/articles/103371.pdf
- Data publikacji:
- 2018
- Wydawca:
- Stowarzyszenie Inżynierów i Techników Mechaników Polskich
- Tematy:
-
buckling
finite elements method
nonlinear analysis
polycarbonate
experimental stand
stress distributions
wyboczenie
metoda elementów skończonych
analiza nieliniowa
poliwęglan
stojak doświadczalny
rozkłady naprężeń - Opis:
- The paper presents results of research on thin-walled load-bearing structure model representing a fragment of plane wing torsion box. The basis for obtaining data on deformation character and stability loss process was a model experiment conducted using a dedicated experimental stand. On the basis of experiment results, adequate numerical simulations were conducted using software based on finite elements method. Results of non-linear numerical analyses allowed to determine the character of stress distribution and formulate conclusions regarding behaviour of the post-critical deformations of the examined wing part.
- Źródło:
-
Advances in Science and Technology. Research Journal; 2018, 12, 3; 203-209
2299-8624 - Pojawia się w:
- Advances in Science and Technology. Research Journal
- Dostawca treści:
- Biblioteka Nauki
Artykuł