Finite-element modeling of the heat mode of autoclave hardening of a three-layer panel

被引：0

作者：

Tatarnikov O.V. ^{[1
]}

Malysheva G.V. ^{[2
]}

Akhmetova E.S. ^{[2
]}

Morozov B.B. ^{[3
]}

机构：

[1] Plekhanov Russian Economical University, Stremyannyi per. 36, Moscow

[2] Bauman Moscow State Technical University, Vtoraya Baumanskaya ul. 5, Moscow

[3] PAO Sukhoi, ul. Polikarpova 23B, PO Box 604, Moscow

来源：

Malysheva, G.V. (malyin@mail.ru) | 1600年 / Maik Nauka Publishing / Springer SBM卷 / 09期

关键词：

finite-element method; hardening; heat mode; honeycomb panel; three-layer panel;

D O I：

10.1134/S1995421216010226

中图分类号：

学科分类号：

摘要：

Results of finite-element modeling and experimental measurements of temperatures in the course of autoclave hardening of a three-layer panel of the wing of a T-50 aircraft, which is composed of upper and lower load-bearing panels made of carbon plastics and honeycomb from aluminum foil, are given. It is shown that the actual temperature values at various sections of the panel of wing differ from the theoretical ones by less than 90%. © 2016, Pleiades Publishing, Ltd.

引用

页码：13 / 16

页数：3

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