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Sergey V.

FEM of the test wing box of IL-86 aircraft

by Sergey V., last login 611 days ago

FEM of the test wing box of IL-86 aircraft  Finite element analysis of the test wing box of IL-86 heavy aircraft. Obtained stresses and calculated durability of longitudinal joints were confirmed with real tensometric data and crack propagation logs. FEM |  FEA |  strength |  stress |  durability |  tensometry
Description
Finite element analysis of the test wing box of IL-86 heavy aircraft. Obtained stresses and calculated durability of longitudinal joints were confirmed with real tensometric data and crack propagation logs.
Tags
FEM FEA strength stress durability tensometry
176985602337900
Last Item
UA
Sergey V.

Sergey V.

Structural Analysis, English, CorelDraw
Kharkov, Kharkivska
4.8
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About Sergey V.
I work in the field of aircraft durability and strength. I can perform works related with cad (3d, 2d modeling using solidworks), cae (fea using ansys, cosmos), research works.
Sergey V. | Elance

Sergey V.