Abstract: This document presents the methodology which was adopted to optimize the performance of cradle of a rocket launcher designed for military applications. The cradle was modelled and transient analysis was conductedusing ANSYS with various combinations of design parameters using standard orthogonal arrays as proposed by Taguchi.Design variables like plate thicknesses are optimized so as to reduce the weight while keeping the equivalent stresses and deformation incurred within the limits.
Keywords: DOE, finite element analysis, frame,Taguchi, weight optimization
[1] Tushar M. Patel, Dr. M. G. Bhatt, Harshad K. Patel, Parametric Optimization of Eicher 11.10 Chassis Frame for Weight Reduction Using FEA-DOE Hybrid Modeling, IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE) e-ISSN: 2278-1684,p-ISSN: 2320-334X, Volume 6, Issue 2 (Mar. - Apr. 2013), PP 92-100
[2] Stephanie Fraley, Mike Oom, Ben Terrien, John Zalewski, Design of experiments via taguchi methods: orthogonal arrays, 2007
[3] Madhu Kiran Karanam, Seetharama Manthri, Chakradhari Bajpai, Weight Optimization of converter housing using Altair Hyperstudy, Altair Technology Conference, 2013
[4] Wen-Hsien Hsua, Ching-Kong Chaoa, Hsi-Ching Hsub, Jinn Lin b, Ching-Chi Hsua, Parametric study on the interface pullout strength of the vertebral body replacement cage using FEM-based Taguchi methods, Medical Engineering & Physics 31, 2009, 287–294. [5] Bappa Acherjee, Arunanshu S. Kuar, Souren Mitra, Dipten Misra, Modeling of laser transmission contour welding process using FEA and DoE, Optics & Laser Technology 44-5, 2012 1281-1289