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...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | Russian |
| Published: |
Moscow State Technical University of Civil Aviation
2017-06-01
|
| Series: | Научный вестник МГТУ ГА |
| Subjects: | |
| Online Access: | https://avia.mstuca.ru/jour/article/view/1087 |