The influence of unsteady streaks on the stability of flat plate boundary layers
Author(s)
Vaughan, Nicholas James
Type
Thesis
Abstract
The natural mechanism for transition to turbulence in flat-plate boundary layers is the
growth and breakdown of Tollmien-Schlichting (TS) waves. In the presence of significant
free-stream turbulence (FST) however, streamwise velocity perturbations, known as Klebanoff
modes or streaks, amplify inside the boundary layer. These distortions alter the
stability characteristics of the boundary layer, and the natural mechanism is bypassed,
leading to earlier transition.
Herein, a model is employed to describe the Klebanoff distortions: one Fourier component
of the FST is used along with its signature inside the shear region to force the boundary
layer and stimulate streaks. Varying the parameters of the forcing mode causes streaks with
different frequencies and amplitudes. A base flow which is periodic in two dimensions is
formed, and its linear stability is investigated using Floquet theory. Two modes emerge as
the most unstable, and their eigenvalues are tracked whilst varying streak frequency and
amplitude. The ‘inner’ mode, is related to the TS wave, but its growth rate is enhanced
by unsteady streaks. The ‘outer’ mode is a high-frequency instability of the streaks at the
edge of the boundary layer. It has no counterpart in the undisturbed boundary-layer. The
critical streak amplitude for the outer mode is calculated for different streak frequencies and
it agrees more closely with experiments than previous analyses which assumed the streaks
to be steady. The current analysis indicates that increasing the frequency of the streaks can
enhance their instability. In fact an optimum frequency exists for free-stream disturbances
to penetrate the shear and stimulate unstable streaks.
Direct numerical simulations with streaks and secondary-instability eigenmodes are conducted.
The simulations show that both the inner and outer mode can grow to nonlinear
amplitudes and cause boundary-layer transition to turbulence.
growth and breakdown of Tollmien-Schlichting (TS) waves. In the presence of significant
free-stream turbulence (FST) however, streamwise velocity perturbations, known as Klebanoff
modes or streaks, amplify inside the boundary layer. These distortions alter the
stability characteristics of the boundary layer, and the natural mechanism is bypassed,
leading to earlier transition.
Herein, a model is employed to describe the Klebanoff distortions: one Fourier component
of the FST is used along with its signature inside the shear region to force the boundary
layer and stimulate streaks. Varying the parameters of the forcing mode causes streaks with
different frequencies and amplitudes. A base flow which is periodic in two dimensions is
formed, and its linear stability is investigated using Floquet theory. Two modes emerge as
the most unstable, and their eigenvalues are tracked whilst varying streak frequency and
amplitude. The ‘inner’ mode, is related to the TS wave, but its growth rate is enhanced
by unsteady streaks. The ‘outer’ mode is a high-frequency instability of the streaks at the
edge of the boundary layer. It has no counterpart in the undisturbed boundary-layer. The
critical streak amplitude for the outer mode is calculated for different streak frequencies and
it agrees more closely with experiments than previous analyses which assumed the streaks
to be steady. The current analysis indicates that increasing the frequency of the streaks can
enhance their instability. In fact an optimum frequency exists for free-stream disturbances
to penetrate the shear and stimulate unstable streaks.
Direct numerical simulations with streaks and secondary-instability eigenmodes are conducted.
The simulations show that both the inner and outer mode can grow to nonlinear
amplitudes and cause boundary-layer transition to turbulence.
Date Issued
2010-09
Date Awarded
2011-09
Copyright Statement
Attribution NoDerivatives 4.0 International Licence (CC BY-ND)
Advisor
Zaki, Tamer
Sponsor
EPSRC
Creator
Vaughan, Nicholas James
Publisher Department
Mechanical Engineering
Publisher Institution
Imperial College London
Qualification Level
Doctoral
Qualification Name
Doctor of Philosophy (PhD)