Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
Propellant injection velocity effect on screech in 20,000 pound hydrogen-oxygen rocket engin
Injector radial distribution and thrust chamber geometry effect on acoustic mode instability in hydr...
Coaxial injector thrust effects on combustion stability of hydrogen-oxygen rocket engin
Test firings and analytical model used to evaluate chugging instability in subscale experiments with...
Liquid oxygen set behavior during combustion instability in gaseous hydrogen fueled rocket combusto
The combustion stability characteristics of a combustor consisting of a single shear element and a c...
Chamber pressure, contraction ratio, and flow per element effects on acoustic mode instability in hy...
Stability effects of several injector face baffle configurations on screech in hydrogen-oxygen rocke
An analytical technique was developed to solve nonlinear longitudinal combustion instability problem...
Oscillatory combustion of liquid oxygen jet with diffusely injected gaseous hydroge
Ablative and steel chambers effect on combustion instability in hydrogen oxygen rocket engin
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
A technique for predicting the stability characteristics of a gaseous-propellant rocket combustion s...
Ignition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen p...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
Propellant injection velocity effect on screech in 20,000 pound hydrogen-oxygen rocket engin
Injector radial distribution and thrust chamber geometry effect on acoustic mode instability in hydr...
Coaxial injector thrust effects on combustion stability of hydrogen-oxygen rocket engin
Test firings and analytical model used to evaluate chugging instability in subscale experiments with...
Liquid oxygen set behavior during combustion instability in gaseous hydrogen fueled rocket combusto
The combustion stability characteristics of a combustor consisting of a single shear element and a c...
Chamber pressure, contraction ratio, and flow per element effects on acoustic mode instability in hy...
Stability effects of several injector face baffle configurations on screech in hydrogen-oxygen rocke
An analytical technique was developed to solve nonlinear longitudinal combustion instability problem...
Oscillatory combustion of liquid oxygen jet with diffusely injected gaseous hydroge
Ablative and steel chambers effect on combustion instability in hydrogen oxygen rocket engin
Liquid rocket acoustic instability for hydrogen-oxygen and earth storable propellant combination
A technique for predicting the stability characteristics of a gaseous-propellant rocket combustion s...
Ignition performance and operating characteristics of oxidizer-rich liquid oxygen/gaseous hydrogen p...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
Propellant injection velocity effect on screech in 20,000 pound hydrogen-oxygen rocket engin
Injector radial distribution and thrust chamber geometry effect on acoustic mode instability in hydr...