EXTRUSION FORMING OF A DOUBLE BASE SOLID ROCKET PROPELLANT BY FINITE ELEMENT METHOD
| Autor: | Barış KALAYCIOĞLU, M. Hüsnü DİRİKOLU, Veli ÇELİK |
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| Jazyk: | English<br />Turkish |
| Rok vydání: | 2007 |
| Předmět: | |
| Zdroj: | Pamukkale University Journal of Engineering Sciences, Vol 13, Iss 1, Pp 31-37 (2007) |
| Druh dokumentu: | article |
| ISSN: | 1300-7009 2147-5881 |
| Popis: | In this study, three dimensional modelling of extrusion forming of a double base solid rocket propellant is performed on Ansys® finite element simulation package. For the purpose of initial model construction and later comparisons with elastoviscoplastik model, the solid propellant is assumed to obey the elastic-plastic material response during the direct extrusion process. Taking into account the contact surface behavior with Coulomb friction and geometric and material nonlinearities, an incremental large large strain solution methodology has been adapted in the simulation. The hydrostatic pressure, stress, strain, and displacement values during extrusion of the solid rocket propellant are obtained from the simulation. |
| Databáze: | Directory of Open Access Journals |
| Externí odkaz: |
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