INVESTIGATION OF THE STRESS-STRAIN STATE OF THE CONSOLE WITH HOLE

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Abstract


The paper presents an analytical model estimates the stress-strain state and stability of the wing with a cutout, built on the basis of the energy method. The results of the calculations and their comparison with the results obtained by the finite element. Obtained in this study are calculated according to analytical.

About the authors

S E Zaytsev

ООО “ANT-Inform”

Email: SergeyE.Z@yandex.ru

V S Safronov

Moskovskiy aviatsionniy institute (GTU)

Email: v.s.safronov@mail.ru

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