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Computation of the POGO self-oscillation parameters in the dynamic "propulsion – rocket structure" system by using a 3d structural model
A mathematical model describing the nonlinear dynamical interaction of a launch vehicle (LV) and its marching liquid-propellant engine in the active phase of the LV flight is developed on the basis of the finiteelement discretization of the "propulsion – LV structure" self-oscillating syst...
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| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Інститут технічної механіки НАН України і НКА України
2018
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| Series: | Технічна механіка |
| Online Access: | http://dspace.nbuv.gov.ua/handle/123456789/173894 |
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