Characterisation and estimation of the flow over a forward-facing step
Author(s)
Pearson, David Stanley
Type
Thesis
Abstract
The turbulent flow over a forward-facing step is studied using two-dimensional time-resolved
Particle Image Velocimetry and simultaneously sampled wall-pressure fluctuations.
The structure and behaviour of the separation region in front of the step
is investigated using conditional averages based on the area of reverse flow present.
The relation between the position of upstream separation and the two-dimensional
shape of the separation region is presented. It is shown that when of ‘closed’ form,
the separation region can become unstable resulting in the ejection of fluid over the
corner of the step. The conditional averages are traced backwards in time to identify
the average behaviour of the boundary layer displacement thickness leading up to
such events. It is shown that these ejections are preceded by the convection of low
velocity regions from upstream, resulting in a three-dimensional interaction within
the separation region. The ejections are also shown to be linked to instances of increased
swirling motion downstream. A mechanism for this process is proposed based
on observations of the flow angle and magnitude over the step corner.
The velocity field is then estimated using wall-pressure measurements. A linear model
of the flow is created using Optimal Mode Decomposition (OMD), which is a generalisation
of Dynamic Mode Decomposition (DMD). A comparison between OMD and
DMD is made using both a synthetic waveform and the PIV data. In both instances
it is shown to provide a model with a lower residual error and, for the synthetic waveform,
an improved estimate of the system eigenvalues. The weights of the OMD modes
are then used as the system states in a Kalman Filter with the pressure measurements
as the system output. The performance of the Kalman Filter is shown to be superior
to that of pseudo-inverse techniques such as Linear Stochastic Estimation.
Particle Image Velocimetry and simultaneously sampled wall-pressure fluctuations.
The structure and behaviour of the separation region in front of the step
is investigated using conditional averages based on the area of reverse flow present.
The relation between the position of upstream separation and the two-dimensional
shape of the separation region is presented. It is shown that when of ‘closed’ form,
the separation region can become unstable resulting in the ejection of fluid over the
corner of the step. The conditional averages are traced backwards in time to identify
the average behaviour of the boundary layer displacement thickness leading up to
such events. It is shown that these ejections are preceded by the convection of low
velocity regions from upstream, resulting in a three-dimensional interaction within
the separation region. The ejections are also shown to be linked to instances of increased
swirling motion downstream. A mechanism for this process is proposed based
on observations of the flow angle and magnitude over the step corner.
The velocity field is then estimated using wall-pressure measurements. A linear model
of the flow is created using Optimal Mode Decomposition (OMD), which is a generalisation
of Dynamic Mode Decomposition (DMD). A comparison between OMD and
DMD is made using both a synthetic waveform and the PIV data. In both instances
it is shown to provide a model with a lower residual error and, for the synthetic waveform,
an improved estimate of the system eigenvalues. The weights of the OMD modes
are then used as the system states in a Kalman Filter with the pressure measurements
as the system output. The performance of the Kalman Filter is shown to be superior
to that of pseudo-inverse techniques such as Linear Stochastic Estimation.
Date Issued
2012-12
Date Awarded
2013-06
Copyright Statement
Attribution NoDerivatives 4.0 International Licence (CC BY-ND)
Advisor
Goulart, Paul
Sponsor
Engineering and Physical Sciences Research Council ; European Union
Grant Number
EP/F056206/1
FP7-ICT- 2009-4 248940
Publisher Department
Aeronautics
Publisher Institution
Imperial College London
Qualification Level
Doctoral
Qualification Name
Doctor of Philosophy (PhD)