Dynamic behavior of wing leading edge assembly with thermal protection coating


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

详细

The paper presents an approximate solution of a problem on dynamic behavior of a wing leading edge assembly discretely reinforced by a system of ribs and coated with thermal protection coating.

作者简介

B. Antuf’ev

Moscow Aviation Institute (National Research University)

编辑信件的主要联系方式.
Email: antufjev.bor@yandex.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993

补充文件

附件文件
动作
1. JATS XML

版权所有 © Allerton Press, Inc., 2017