Static Structural Analysis and Static Fluid Pressurized on Marlin Glider Wing Torpedo’s

International Journal of Mechanical Engineering
© 2023 by SSRG - IJME Journal
Volume 10 Issue 12
Year of Publication : 2023
Authors : Pothuraju V V Satyanarayana, Kamalakar Kasimahanti, Vivek Sachan, Hari Kishan Mantravadi
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How to Cite?

Pothuraju V V Satyanarayana, Kamalakar Kasimahanti, Vivek Sachan, Hari Kishan Mantravadi, "Static Structural Analysis and Static Fluid Pressurized on Marlin Glider Wing Torpedo’s," SSRG International Journal of Mechanical Engineering, vol. 10,  no. 12, pp. 1-5, 2023. Crossref, https://doi.org/10.14445/23488360/IJME-V10I12P101

Abstract:

The design technique for the glider wing torpedo is open to design parameter changes and gives the designer insight into the security of the final configuration. Constructing a torpedo finite element model and testing its static properties as a function of design parameters structural analysis of torpedo’s were significantly used to strengthen our defence system. In this paper, three models, circular, elliptical and black marlin glider wing torpedoes, were introduced, and the results of the three models were compared at static load and pressure conditions. The parameters were taken at the deepest point of the Pacific Ocean under standard conditions. The black marlin glider wing torpedo shows better results than the other two models.

Keywords:

Glider wing, Strengthen, Static load, Static pressure, Pacific Ocean standards.

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