An analytical technique for the calculation of linear decay coefficients in combustors with acoustic...
Behavior of convergent-divergent nozzles and acoustic liners in three dimensional acoustic field
Operation manual for steady state resonance tests through flow at rocket motor acoustic test facilit
Static rocket thrust chamber simulator for cylindrical cold flow-type apparatus desig
Nonarray absorbing devices were investigated for use in rocket thrust chambers as instability suppre...
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Hydrogen-oxygen rocket engine used to test acoustic liner with isolated resonators and variable cavi...
Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket eng...
Computerized simulation of high frequency instability in gas in liquid propellant rocket engine
Experimental, and theoretical evaluations of acoustic liners for screech suppression in rocket engin...
Helmholtz resonators with variable cavity depths tested with unstable rocket combusto
Characterization of pressure perturbations induced in rocket combustor by machine gu
Combustion instabilities in rocket engines are caused by coupling between the combustion processes a...
A series of rocket motor firings was performed in a modified linear aerospike thrust chamber with th...
The theory and procedures for determining the characteristics of pressure oscillations in rocket eng...
An analytical technique for the calculation of linear decay coefficients in combustors with acoustic...
Behavior of convergent-divergent nozzles and acoustic liners in three dimensional acoustic field
Operation manual for steady state resonance tests through flow at rocket motor acoustic test facilit
Static rocket thrust chamber simulator for cylindrical cold flow-type apparatus desig
Nonarray absorbing devices were investigated for use in rocket thrust chambers as instability suppre...
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Hydrogen-oxygen rocket engine used to test acoustic liner with isolated resonators and variable cavi...
Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket eng...
Computerized simulation of high frequency instability in gas in liquid propellant rocket engine
Experimental, and theoretical evaluations of acoustic liners for screech suppression in rocket engin...
Helmholtz resonators with variable cavity depths tested with unstable rocket combusto
Characterization of pressure perturbations induced in rocket combustor by machine gu
Combustion instabilities in rocket engines are caused by coupling between the combustion processes a...
A series of rocket motor firings was performed in a modified linear aerospike thrust chamber with th...
The theory and procedures for determining the characteristics of pressure oscillations in rocket eng...
An analytical technique for the calculation of linear decay coefficients in combustors with acoustic...
Behavior of convergent-divergent nozzles and acoustic liners in three dimensional acoustic field
Operation manual for steady state resonance tests through flow at rocket motor acoustic test facilit