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Numerical Validation of Octopus Wheel Rim using FEA
Details
Numerical prediction of the stress response of an octopus-type spoked wheel under steady state (static) loading conditions is carried out using commercially available FEA software. The model used in the simulation is based on the wheel model experimented on by H.Akbulut. The boundary and the loading conditions are same as those used in the measurement so as to enable comparison of the numerical results with measurement data and hence validate them.The geometry of the wheel is symmetric about the two Cartesian axes and hence only a quarter of the wheel is modeled for analysis. An optimum mesh size was arrived at starting from a coarse mesh,the mesh used for the final run involved hexa and penta elements. The simulation is carried out on the part, where spoke is connected to rim as it is the critical region and the plastic regions develop in the vicinity of the critical zone for higher loads. The computational results indicate that the design is safe for a load less than or equal to 16.3 kN. The numerically predicted stress response is compared with measurement data of H.Akbulut. It is observed that the numerical prediction agrees reasonably well with the experimental results.
Autorentext
Mr. Somanatha. M has done his engineering in mechanical engineering stream from BIT, Bangalore. At present he is doing his masters in machine design stream from AMC College of engineering, Bangalore. He has also worked has quality engineer in Nash Products and carried out several research work related to mechanical components.
Weitere Informationen
- Allgemeine Informationen
- GTIN 09783659696053
- Sprache Englisch
- Genre Maschinenbau
- Anzahl Seiten 88
- Größe H220mm x B150mm x T6mm
- Jahr 2015
- EAN 9783659696053
- Format Kartonierter Einband
- ISBN 3659696056
- Veröffentlichung 21.04.2015
- Titel Numerical Validation of Octopus Wheel Rim using FEA
- Autor Somanatha M. , Avinash L. , Manjunatha N.
- Untertitel Steady state static analysis of Octopus Wheel Rim
- Gewicht 149g
- Herausgeber LAP LAMBERT Academic Publishing