A Customized Wavelet-Based Hierarchical A Posteriori Error Indicator for Linear and Nonlinear PDES
Journal Title: International Journal of Mechanical and Production Engineering Research and Development (IJMPERD ) - Year 2019, Vol 9, Issue 4
Abstract
This paper presents an adaptive method that can be used to improve the finite element solution of a linear or non-linear PDE by indicating the local as well as global errors. This wavelet-based adaptation is based on hierarchical finite element error estimation scheme. The finite element solution of engineering problems is transformed into the multilevel decomposition of wavelet space. The functions of wavelets coefficient are used as an a posteriori error indicator. The error estimations in the present setting do not have any problem due to the complex domain of engineering structures and is applicable in some small region as well as the complete domain. The proposed technique is quite efficient for linear problems like structures with discontinuity as well as non-linear ones such as contact problem.
Authors and Affiliations
Kumar Kaushik Ranjan, Ambuj Sharma, Sandeep Kumar, Amit Tyagi
Impact Analysis of ISO 9001 Certification on Service Companies in Indonesia Using PLS-Sem
More than one million organizations in the world has certified ISO 9001 to improve their performance related to quality, productivity and cost efficiency. The purpose of this study is to confirm that certification of ISO...
A Small-Scale Fabrication Facility for Extraction of Alternative Diesel Fuel from Waste Plastic
Plastic waste is viewed as conceivably economy wellspring of chemicals and vitality. Because of the expanding level of private utilization of these plastic materials, colossal measures of squanders are released to the ea...
Design of Transmission System for a Hybrid Vehicle
Conventional vehicles use gasoline or diesel to power an internal combustion engine which produces harmful gases into the environment. The best way to overcome this problem is by using a hybrid vehicle. The goal of a hyb...
Aero-Structural Optimization of Aircraft Wing by Finite Element Method
New and innovative designs must be explored to meet the aircraft requirements lower weight and more cost effective structure for future airplanes. For these reasons, present study aims to deals with the structural analys...
Numerical Analysis of Flow Over NACA0012 at Fixed Mach Number using Computational Fluid Dynamics
In this present work, we carry out a numerical analysis of lift and drag performances of NACA0012 airfoil at various angles of attack, by using computational fluid dynamic software. We can also utilize wind tunnel testin...