KFU. Card publication. Stability of a cylindrical shell under axial compression

KAZAN
FEDERAL UNIVERSITY

- RUS
- 中文
- ES

STABILITY OF A CYLINDRICAL SHELL UNDER AXIAL COMPRESSION

Form of presentation

Articles in international journals and collections

Year of publication

2015

Язык

английский

Authors, employees of KFU

Bakhtieva Lyalya Uzbekovna, author

Tazyukov Ferid Khosnutdinovich, author

Bibliographic description in the original language

Bakhtieva, L.U., Tazyukov, F.K. Stability of a cylindrical shell under axial compression // Russian Aeronautics (Iz. VUS). - 2015. - 58 (1), pp. 106-111.

Annotation

A new approach to solving the task of stability for a circular cylindrical shell under axial compression is presented, taking into account the dynamic buckling. The modification of the algorithm for solving the known problem by the Ritz method is also proposed that allows investigating the effect of geometrical factors on the buckling load.

Keywords

buckling load, deflection, shell, stability

The name of the journal

Russian Aeronautics (Iz. VUS)

Please use this ID to quote from or refer to the card

https://repository.kpfu.ru/eng/?p_id=126323&p_lang=2

Resource files

File name	Size (MB)	Format
17_Bakhtieva.pdf	0,25	pdf	show / download

Full metadata record

Field DC	Value	Language
dc.contributor.author	Bakhtieva Lyalya Uzbekovna	ru_RU
dc.contributor.author	Tazyukov Ferid Khosnutdinovich	ru_RU
dc.date.accessioned	2015-01-01T00:00:00Z	ru_RU
dc.date.available	2015-01-01T00:00:00Z	ru_RU
dc.date.issued	2015	ru_RU
dc.identifier.citation	Bakhtieva, L.U., Tazyukov, F.K. Stability of a cylindrical shell under axial compression // Russian Aeronautics (Iz. VUS). - 2015. - 58 (1), pp. 106-111.	ru_RU
dc.identifier.uri	https://repository.kpfu.ru/eng/?p_id=126323&p_lang=2	ru_RU
dc.description.abstract	Russian Aeronautics (Iz. VUS)	ru_RU
dc.description.abstract	A new approach to solving the task of stability for a circular cylindrical shell under axial compression is presented, taking into account the dynamic buckling. The modification of the algorithm for solving the known problem by the Ritz method is also proposed that allows investigating the effect of geometrical factors on the buckling load.	ru_RU
dc.language.iso	ru	ru_RU
dc.subject	buckling load	ru_RU
dc.subject	deflection	ru_RU
dc.subject	shell	ru_RU
dc.subject	stability	ru_RU
dc.title	Stability of a cylindrical shell under axial compression	ru_RU
dc.type	Articles in international journals and collections	ru_RU