电邮这篇文章 The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties
- 作者: Bakulin V.N.1, Vinogradov Y.I.2, Men’kov G.B3
-
隶属关系:
- Institute of Applied Mechanics
- Bauman Moscow State Technical University
- Russian State Social University
- 期: 卷 61, 编号 2 (2018)
- 页面: 156-164
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230464
- DOI: https://doi.org/10.3103/S1068799818020022
- ID: 230464
如何引用文章
开放存取
##reader.subscriptionAccessGranted##
订阅存取
详细
The equations of the mathematical model are solved in terms of special functions. The results for the design scheme of the aircraft forebody are obtained with a guaranteed accuracy by the stable method of functional normalization.
作者简介
V. Bakulin
Institute of Applied Mechanics
编辑信件的主要联系方式.
Email: vbak@yandex.ru
俄罗斯联邦, Leningradskii pr. 7, Moscow, 125040
Yu. Vinogradov
Bauman Moscow State Technical University
Email: vbak@yandex.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
G. Men’kov
Russian State Social University
Email: vbak@yandex.ru
俄罗斯联邦, ul. Wilhelm Pick 4, Moscow, 129226
补充文件
