Email this article The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties
- Authors: Bakulin V.N.1, Vinogradov Y.I.2, Men’kov G.B3
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Affiliations:
- Institute of Applied Mechanics
- Bauman Moscow State Technical University
- Russian State Social University
- Issue: Vol 61, No 2 (2018)
- Pages: 156-164
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/230464
- DOI: https://doi.org/10.3103/S1068799818020022
- ID: 230464
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Abstract
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.
About the authors
V. N. Bakulin
Institute of Applied Mechanics
Author for correspondence.
Email: vbak@yandex.ru
Russian Federation, Leningradskii pr. 7, Moscow, 125040
Yu. I. Vinogradov
Bauman Moscow State Technical University
Email: vbak@yandex.ru
Russian Federation, ul. 2-ya Baumanskaya 5, Moscow, 105005
G. B Men’kov
Russian State Social University
Email: vbak@yandex.ru
Russian Federation, ul. Wilhelm Pick 4, Moscow, 129226
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