DYNAMIC LOAD OF THE THIN CONICAL RADOME WITH A CONSIDERATION OF ATTACHED ADDITIONAL MASS
At the present stage of aviation and missile equipment development there is increasing necessity for considering fast-acting, high-speed processes of impact interaction of structure elements with external loads, represented as both power factors (longitudinal force or bending moment) and uniformly s...
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| Main Authors: | , |
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| Format: | Article |
| Language: | Russian |
| Published: |
Moscow State Technical University of Civil Aviation
2017-06-01
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| Series: | Научный вестник МГТУ ГА |
| Subjects: | |
| Online Access: | https://avia.mstuca.ru/jour/article/view/1087 |
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