Paper presents a numerical simulation of the occurrence of flow instability and pressure self-oscillations for a complex configuration of the gas-dynamic tract in combustion chamber. Unsteady axisymmetric two-dimensional Navier-Stokes equations are used for mathematical modelling of compressible one-phase medium. To simulate turbulence, the k-ε and LES models were used. Fast Fourier Transform (FFT) determined the frequency spectrum of pressure pulsations in the combustion chamber. It is shown that in the case of a simple geometry of the free gas cavity in combustion chamber, both models of turbulence make it possible to determine the spectrum of the natural acoustic frequencies. Using the LES model in the case of complex geometry makes it p...
Combustion instabilities are strong acoustic disturbances that often form spontaneously inside rocke...
The overall objective of the current research is to evaluate if and how computational fluid dynamics...
In the paper the real oscillatory process is reproduced by statement of direct numerical experiment ...
Paper presents a numerical simulation of the occurrence of flow instability and pressure self-oscill...
Numerical simulation of the flow instability and pressure self-oscillations for complex configuratio...
Currently, gas turbine manufacturers frequently face the problem of strong acoustic combustion-drive...
Combustion instability in rocket engines is accompanied by large-amplitude pressure fluctuations in ...
An analytical and experimental study is being made of the role of combustion in large vortical struc...
High frequency combustion instability has recently been observed by Rocketdyne in a 40K thrust metha...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
High frequency combustion instabilities in liquid propellant rocket engines are spontaneously occurr...
old gas scale model experiments (1/30) demonstrate that coupling of vortex shedding with acoustic st...
A numerical analysis of unsteady motions in solid rocket motors has been conducted. A fully coupled ...
The unstable combustion that can occur in combustion chambers is a major problem for aeroengines and...
Currently, gas turbine manufacturers frequently face the problem of strong acoustic combustion-drive...
Combustion instabilities are strong acoustic disturbances that often form spontaneously inside rocke...
The overall objective of the current research is to evaluate if and how computational fluid dynamics...
In the paper the real oscillatory process is reproduced by statement of direct numerical experiment ...
Paper presents a numerical simulation of the occurrence of flow instability and pressure self-oscill...
Numerical simulation of the flow instability and pressure self-oscillations for complex configuratio...
Currently, gas turbine manufacturers frequently face the problem of strong acoustic combustion-drive...
Combustion instability in rocket engines is accompanied by large-amplitude pressure fluctuations in ...
An analytical and experimental study is being made of the role of combustion in large vortical struc...
High frequency combustion instability has recently been observed by Rocketdyne in a 40K thrust metha...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
High frequency combustion instabilities in liquid propellant rocket engines are spontaneously occurr...
old gas scale model experiments (1/30) demonstrate that coupling of vortex shedding with acoustic st...
A numerical analysis of unsteady motions in solid rocket motors has been conducted. A fully coupled ...
The unstable combustion that can occur in combustion chambers is a major problem for aeroengines and...
Currently, gas turbine manufacturers frequently face the problem of strong acoustic combustion-drive...
Combustion instabilities are strong acoustic disturbances that often form spontaneously inside rocke...
The overall objective of the current research is to evaluate if and how computational fluid dynamics...
In the paper the real oscillatory process is reproduced by statement of direct numerical experiment ...