Add to ORKGDesign criteria, methods and data, were developed to permit effective design of acoustic cavities fo...
Theoretical studies and test facility installation for investigating behavior of rocket nozzles and ...
Stability effects of several injector face baffle configurations on screech in hydrogen-oxygen rocke
Helmholtz resonators with variable cavity depths tested with unstable rocket combusto
Experimental investigation of acoustic liners to suppress screech in hydrogen-oxygen engine
Experimental, and theoretical evaluations of acoustic liners for screech suppression in rocket engin...
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Mechanical absorption of acoustic oscillations in simulated rocket combustion chamber
A series of rocket motor firings was performed in a modified linear aerospike thrust chamber with th...
Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket eng...
Testing Helmholtz resonator arrays in rocket engine and cold flow testing of single Helmholtz resona...
The feasibility of damping more than one mode of rocket engine combustion instability by means of di...
Behavior of convergent-divergent nozzles and acoustic liners in three dimensional acoustic field
Acoustic liner for controlling combustion instability in rocket engines using ablative chamber
Four liners are investigated experimentally via tests in the NASA Langley Grazing Flow Impedance Tub...
Design criteria, methods and data, were developed to permit effective design of acoustic cavities fo...
Theoretical studies and test facility installation for investigating behavior of rocket nozzles and ...
Stability effects of several injector face baffle configurations on screech in hydrogen-oxygen rocke
Helmholtz resonators with variable cavity depths tested with unstable rocket combusto
Experimental investigation of acoustic liners to suppress screech in hydrogen-oxygen engine
Experimental, and theoretical evaluations of acoustic liners for screech suppression in rocket engin...
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
Mechanical absorption of acoustic oscillations in simulated rocket combustion chamber
A series of rocket motor firings was performed in a modified linear aerospike thrust chamber with th...
Stabilizing influence of acoustic cavities on acoustic modes of combustion instability in rocket eng...
Testing Helmholtz resonator arrays in rocket engine and cold flow testing of single Helmholtz resona...
The feasibility of damping more than one mode of rocket engine combustion instability by means of di...
Behavior of convergent-divergent nozzles and acoustic liners in three dimensional acoustic field
Acoustic liner for controlling combustion instability in rocket engines using ablative chamber
Four liners are investigated experimentally via tests in the NASA Langley Grazing Flow Impedance Tub...
Design criteria, methods and data, were developed to permit effective design of acoustic cavities fo...
Theoretical studies and test facility installation for investigating behavior of rocket nozzles and ...
Stability effects of several injector face baffle configurations on screech in hydrogen-oxygen rocke