Design And Analysis Of Bolted Joint For Rocket Motor Casing

被引：5

作者：

Babu, Kondru Nagendra ^{[1
]}

Naresh, Hazari ^{[1
]}

Gupta, G. Srinivasa ^{[1
]}

机构：

[1] Vnr Vignanajothi Inst Engn & Technol, Hyderabad 500090, Andhra Prades, India

来源：

MATERIALS TODAY-PROCEEDINGS | 2018年 / 5卷 / 02期

关键词：

bolted joint; CATIA V5; ANSYS; 15; E-glass;

D O I：

10.1016/j.matpr.2017.12.098

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

This paper deals with composite joints with double bolted single shear tensile loading for two specimens. The bearing response data from single shear test using two piece specimens has been extensively used in the development of design and allowable data. The objective of the work is to design bolted joint for rocket motor casing by using Standard method. Testing was done according to ASTM D5961: Procedure "B" - the standard test for bearing response of single shear two piece polymer matrix composite laminate. It also includes the manufacturing of composite laminates by studying the properties of E-glass and phenolic resin to enhance the properties by adding filler material. Due to unavailability of S-glass and cost factor, E-glass is selected to make coupons. The other aim of the project is to analyze the design by computational study. The modeling is done by using CATIA V5 and the stress analysis and couple field analysis is done by using ANSYS 15. The analysis is carried to build a finite model for quasi isotropic material, to justify the experimental results (c) 2017 Elsevier Ltd. All rights reserved.

引用

页码：5165 / 5174

页数：10