In 1878, Lord Rayleigh formulated his criterion to explain several examples of acoustic waves excited and maintained by heat addition. It is a qualitative explanation successfully capturing the essence of the phenomena but not providing a basis for quantitative predictions. The widespread appeal of Rayleigh's criterion merits placing this important result on a more rigorous basis. To do so requires careful formulation grounded in the theory of small amplitude motions in a compressible fluid. In this chapter, we review the construction of an approximate analysis and establish the equivalence of Rayleigh's criterion and the condition for linear stability of small amplitude motions. Thus Rayleigh's criterion is formulated explicitly ...
Thermoacoustic instabilities are one of the most challenging problems faced by gas turbine and rocke...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
The stability of systems contafning a beat source is examined from the energy pdnt of view. Rayleigh...
In 1878, Lord Rayleigh formulated his criterion to explain several examples of acoustic waves exci...
International audienceCombustion instabilities in a backward-facing step combustor are numerically s...
Based on spatial and temporal averaging of the conservation equations, an approximate analysis prov...
Due to non-linear loss or gain of energy, unstable oscillations in combustion chambers cannot grow ...
This paper is concerned with the general problem of the nonlinear growth and limiting amplitude of a...
Small amplitude linear analysis of combustion instability with finite Mach number flow and acoustic ...
Unsteady motions in combustion chambers have previously been treated with an approximate analysis in...
For understanding the fundamental properties of unsteady motions in combustion chambers, and for app...
The approximate analysis developed in Part I of Ihis work is apllied to severa1 specific problems. O...
The behavior of unsteady pressure fluctuations in combustion chambers is examined. An approximate me...
Combustion instability (CI) has been persistent in all forms of propulsion since their inception. CI...
Combustion of reactants in a confined volume favors excitation of unsteady motions over a broad rang...
Thermoacoustic instabilities are one of the most challenging problems faced by gas turbine and rocke...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
The stability of systems contafning a beat source is examined from the energy pdnt of view. Rayleigh...
In 1878, Lord Rayleigh formulated his criterion to explain several examples of acoustic waves exci...
International audienceCombustion instabilities in a backward-facing step combustor are numerically s...
Based on spatial and temporal averaging of the conservation equations, an approximate analysis prov...
Due to non-linear loss or gain of energy, unstable oscillations in combustion chambers cannot grow ...
This paper is concerned with the general problem of the nonlinear growth and limiting amplitude of a...
Small amplitude linear analysis of combustion instability with finite Mach number flow and acoustic ...
Unsteady motions in combustion chambers have previously been treated with an approximate analysis in...
For understanding the fundamental properties of unsteady motions in combustion chambers, and for app...
The approximate analysis developed in Part I of Ihis work is apllied to severa1 specific problems. O...
The behavior of unsteady pressure fluctuations in combustion chambers is examined. An approximate me...
Combustion instability (CI) has been persistent in all forms of propulsion since their inception. CI...
Combustion of reactants in a confined volume favors excitation of unsteady motions over a broad rang...
Thermoacoustic instabilities are one of the most challenging problems faced by gas turbine and rocke...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
The stability of systems contafning a beat source is examined from the energy pdnt of view. Rayleigh...