Dynamic behavior of wing leading edge assembly with thermal protection coating
- 作者: Antuf’ev B.A.1
-
隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 60, 编号 1 (2017)
- 页面: 9-12
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229963
- DOI: https://doi.org/10.3103/S1068799817010020
- ID: 229963
如何引用文章
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
