Modeling of periodic non-smooth motion using the harmonic balance method

Master Thesis (2018)
Author(s)

Amey Vasulkar (TU Delft - Electrical Engineering, Mathematics and Computer Science)

Contributor(s)

Duncan van der Heul – Mentor

Faculty
Electrical Engineering, Mathematics and Computer Science
More Info
expand_more
Publication Year
2018
Language
English
Graduation Date
31-08-2018
Awarding Institution
Delft University of Technology
Programme
Applied Mathematics, COSSE (Computer Simulations for Science and Engineering)
Faculty
Electrical Engineering, Mathematics and Computer Science
Downloads counter
213
Collections
thesis
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

The company Deepwater Energy BV, Netherlands developed a unique water turbine called as the Oryon Watermill (OWM). It was the aim of the company to obtain an efficient numerical model for the turbine. A numerical model, which serves as a good starting point, has already been developed by Maniyara [1]. This model suffered from certain limitations and to tackle these it was realized
that a smaller and simpler problem needs to be solved. The current thesis deals with developing a numerical model for this smaller problem.
In this problem, an airfoil is hinged at its leading edge and rotating under the influence of a periodic water flow. Further, the rotation of the airfoil is restricted by a stopper. This restriction leads to a collision between the airfoil and the stopper due to which the motion of the airfoil is changed suddenly. This is a Fluid-Structure Interaction (FSI) problem. To model the structural part i.e. the airfoil motion, a non-smooth dynamical analysis is needed.
Then, the entire FSI problem is solved in a faster and efficient way using the harmonic balance method. For this purpose, the non-smooth dynamics of the airfoil have to be solved using the harmonic balance method. In the thesis, a novel approach is developed to solve the non-smooth dynamics problem using the harmonic balance method. Initially, this new approach is implemented
and verified in MATLAB on a 1D level. Later, a MATLAB-OpenFOAM coupled solver is developed to compute the solution to the airfoil problem using this newly developed approach.

Files

Masters_thesis_Amey.pdf
(pdf | 3.68 Mb)
License info not available