Мақаланы E-mail арқылы жіберу The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties
- Авторлар: Bakulin V.1, Vinogradov Y.2, Men’kov G.3
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Мекемелер:
- Institute of Applied Mechanics
- Bauman Moscow State Technical University
- Russian State Social University
- Шығарылым: Том 61, № 2 (2018)
- Беттер: 156-164
- Бөлім: 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
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
Аннотация
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.
Авторлар туралы
V. Bakulin
Institute of Applied Mechanics
Хат алмасуға жауапты Автор.
Email: vbak@yandex.ru
Ресей, Leningradskii pr. 7, Moscow, 125040
Yu. Vinogradov
Bauman Moscow State Technical University
Email: vbak@yandex.ru
Ресей, ul. 2-ya Baumanskaya 5, Moscow, 105005
G. Men’kov
Russian State Social University
Email: vbak@yandex.ru
Ресей, ul. Wilhelm Pick 4, Moscow, 129226
