Campus Units

Mechanical Engineering, Electrical and Computer Engineering, Aerospace Engineering

Document Type

Conference Proceeding

Conference

28th AIAA Applied Aerodynamics Conference

Publication Version

Published Version

Publication Date

2010

First Page

2010-5078

DOI

10.2514/6.2010-5078

Conference Date

June 28-July 1, 2010

City

Chicago, IL

Abstract

The objective of this paper is to compare the existing methods and develop novel approaches for the experimental data analysis of the unsteady aerodynamics of the flapping wing microaerial-vehicle. These methods are developed for the purpose of identification of the beneficial dynamics and for the development of reduced order models for control design. We first employ Proper Orthogonal Decomposition (POD) method for the data analysis of the PIV measurements in the wakes of piezoelectric flapping wings. The basic idea behind POD based data analysis method is to decompose the time series snapshots of PIV measurements into high energy, POD, modes. The POD modes obtained from the PIV measurement data with different control inputs, such as flapping amplitude, angle of attack and flight speed, are compared to identify high energy modes that are invariant across the range of operating conditions. Similarly the modes that are responsible for maximum energy transfer between the control inputs and the desired output such as lift and thrust are identified. The second method that we propose for the PIV data analysis is inspired from our recent work to develop a novel approach for the spectral analysis of the nonlinear flows. This new method is based on the spectral analysis of the linear transfer operator, the so called Koopman operator, associated with any nonlinear flows. The motivation for this work comes from the desire to perform frequency-based decomposition of the snapshot data as opposed to energy based decomposition in the POD method. While POD-based data analysis method captures all high energy content modes, it ignores the low energy content modes. These low energy modes might play an important role from the dynamics point of view and hence cannot be ignored. We perform the spectral analysis of the linear transfer, Perron-Frobenius (P-F) operator, which is dual to the Koopman operator to obtain the frequency based decomposition of the time series snapshot data. The basic idea behind this approach is to construct the finite dimensional approximation of the linear transfer (P-F) operator that best describes the time evolution of the snapshots data. The eigenvalues and eigenvectors of this transfer operator carry useful information about the system dynamics.

Comments

This proceeding was published as Kai Wang, Umesh Vaidya, Hui Hu, and Baskar Ganapathysubramanian. "Experimental Data Analysis of the Vortex Structures in the Wakes of Flapping Wings", 28th AIAA Applied Aerodynamics Conference, Fluid Dynamics and Co-located Conferences, doi:10.2514/6.2010-5078 . Posted with permission.

Copyright Owner

The Authors

Language

en

File Format

application/pdf

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Article Location

 
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