Add to ORKGCharacteristics of noncircular injector orifices and elements for gas and liquid injector
A conjugate heat transfer computational fluid dynamics (CFD) model to describe regenerative cooling ...
Performance and stability characteristics of rocket engine injectors using liquid oxygen propellan
Evaluating effect of liquid fuel injectants on ablative performance of low cost nozzle material
Results are presented of a cold-flow and hot-fire experimental study of the mixing and atomization c...
Noncircular liquid rocket injector orifices and elements for liquid/liquid propellant
The primary objective was the obtainment of atomization and mixing performance data for a variety of...
Hydraulic characteristics of flow through miniature slot orifices for rocket engine injector
The nozzle is a major component of a rocket engine, having a significant influence on the overall en...
An abbreviated program was conducted to investigate igniter, injector, and thrust chamber technology...
An injector for liquid fueled rocket engines wherein a generally flat core having a frustoconical do...
A high number of liquid oxygen and gaseous hydrogen orifices per unit area are provided in an inject...
Environmental tests on designed hydraulic injector for Apollo service propulsion syste
Apparatus, techniques, and instrumentation for experimental correlation of nonreactive injection sch...
Experimental data are presented for the oblique injection of water and three electrophilic liquids (...
The performance and stability of liquid rocket engines is determined to a large degree by atomizatio...
A conjugate heat transfer computational fluid dynamics (CFD) model to describe regenerative cooling ...
Performance and stability characteristics of rocket engine injectors using liquid oxygen propellan
Evaluating effect of liquid fuel injectants on ablative performance of low cost nozzle material
Results are presented of a cold-flow and hot-fire experimental study of the mixing and atomization c...
Noncircular liquid rocket injector orifices and elements for liquid/liquid propellant
The primary objective was the obtainment of atomization and mixing performance data for a variety of...
Hydraulic characteristics of flow through miniature slot orifices for rocket engine injector
The nozzle is a major component of a rocket engine, having a significant influence on the overall en...
An abbreviated program was conducted to investigate igniter, injector, and thrust chamber technology...
An injector for liquid fueled rocket engines wherein a generally flat core having a frustoconical do...
A high number of liquid oxygen and gaseous hydrogen orifices per unit area are provided in an inject...
Environmental tests on designed hydraulic injector for Apollo service propulsion syste
Apparatus, techniques, and instrumentation for experimental correlation of nonreactive injection sch...
Experimental data are presented for the oblique injection of water and three electrophilic liquids (...
The performance and stability of liquid rocket engines is determined to a large degree by atomizatio...
A conjugate heat transfer computational fluid dynamics (CFD) model to describe regenerative cooling ...
Performance and stability characteristics of rocket engine injectors using liquid oxygen propellan
Evaluating effect of liquid fuel injectants on ablative performance of low cost nozzle material