Combustion is a major source of energy production for a wide range of applications to meet the
increasing demand for power. In recent times, there has been a drive towards clean energy and
lower emissions. Towards this goal, engines are operated under fuel lean conditions, where the
temperature of the products is low, thereby reducing the production of oxides of nitrogen, which
are harmful. However, the development and operation of such engines are marred by the
occurrence of combustion instability (also known as thermoacoustic instability) and blowout of
flame.
Inherent fluctuations in the flow get amplified when the unsteady heat release rate from
combustion interacts in phase with the acoustic field of the combustion chamber. Consequently,
detrimental, high-amplitude, pressure oscillations known as thermoacoustic instability occurs in
combustion systems. These oscillations often cause losses in billions of dollars to the engine
companies. Meanwhile, the blowout of flame is another dangerous problem which can even cause
sudden descent of an airplane, in addition to the financial losses. These detrimental thermoacoustic
instability and flame blowout occur in the system when combustors are operated in a fuel-lean
condition. However, clean combustion as well cannot be avoided to meet the stringent emission
norms. Hence, an understanding of the transition to thermoacoustic instability and blowout is
absolutely critical.
Traditionally, thermoacoustic systems are analyzed from a reductionist approach which
attempts to analyze a complex system in terms of its constituent elements. Recently, it was shown
that the combustion noise and the near blowout dynamics display multifractal characteristics. The
presence of multifractality in the combustion dynamics is a reflection of the complexity of the thermoacoustic systems. The traditional reductionist approach fails to explain the complex
behaviours in the thermoacoustic systems.
In the present thesis, the complex behaviours in the dynamics of thermoacoustic systems are
investigated in the framework of complex networks. First, the pattern in the dynamics of the
combustion noise generated during the stable operation of the combustor is investigated. The
unsteady pressure data from a backward-facing step combustor is converted into obtain complex
networks using the visibility condition. The scale invariance of combustion noise in a confinement
is hard to discern from the frequency spectra due to the presence of low-amplitude peaks, arising
from the coupling of combustion noise with the confinement modes. The complex network
representation reveals the scale invariance of combustion noise as scale-free structure in the
topology of the complex network. The dynamics of the combustion noise is mapped as nodes and
links between them and the power-law behavior in the distribution of links in the network is a clear
reflection of the scale invariant property of the combustion noise generated in a turbulent
environment.
Further, the structure of the complex network during thermoacoustic instability possess regular
topology that represent order. The transition to thermoacoustic instability from combustion noise
is reflected as a transition from scale-free to order in the networks topology. The measures for
quantifying the topological features of the networks such as clustering coefficient, characteristic
path length, network diameter and global efficiency are calculated at each operating conditions
during the transition from combustion noise to thermoacoustic instability. These network measures
change significantly well before the onset of thermoacoustic instability and can be used as the
precursors to thermoacoustic instability.
The transition in the system dynamics from combustion noise to the onset flame blowout is
investigated in the framework of complex networks. The regular structure in the complex networks
during thermoacoustic instability transition to scale-free structure at the onset of blowout. The
network properties are computed and used as the early warning measures to the onset of blowout. The transition to thermoacoustic instability and blowout from the stable operation happened
via intermittency. In order to investigate the physical reasons for such transitions in thermoacoustic
systems, we investigated the intermittent dynamics that presages the onset of thermoacoustic
instability and blowout in a turbulent lifted jet flame combustor. The simultaneous measurement
of acoustic pressure, chemiluminescence images and Mie scattering images are performed in order
to characterize the acoustics-flame-flow interactions during intermittency.
The intermittent dynamics prior to the onset of thermoacoustic instability occurs due to the
alternating (either positively or negatively) coupled interaction of the flame, flow and duct acoustics. In contrast, the intermittency that presages the onset of blowout is caused by the interplay between the blowout precursor events and the driving of high-amplitude pressure oscillations as the flame propagate towards the fuel tube. Alternatively, the commonality between the intermittency prior to thermoacoustic instability and blowout is investigated using first return maps and recurrence plots.
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