Flameholding measurements were made in two different direct connect combustor facilities that were designed to simulate a cavity flameholder in the flowfield of a hydrocarbon fueled dual-mode scramjet combustor. The presence of a shocktrain upstream of the flameholder has a significant impact on the inlet flow to the combustor and on the flameholding limits. A throttle was installed in the downstream end of the test rigs to provide the needed back-pressurization and decouple the operation of the flameholder from the backpressure formed by heat release and thermal choking, as in a flight engine. Measurements were made primarily with ethylene fuel but a limited number of tests were also performed with heated gaseous JP-7 fuel injection. The f...
This study has been conducted in a partial fulfillment of a master of science degree in nuclear engi...
The purpose of the STME Main Injector Program was to enhance the technology base for the large-scale...
A millimeter-wave traveling wave tube (TWT) was developed using a dispersive, high-impedance forward...
An experimental and computational study was conducted on a high-speed, single-expansion-ramp nozzle ...
Recent work has been done with the goal of establishing ultralow emission aircraft gas turbine combu...
The design and development of an airborne flight-test experiment to study nonreacting gas jets injec...
The purpose of this study is to examine the predictive capabilities of fire models using the results...
A comparative study of wall mounted swept ramp injectors fitted with injector nozzles of different s...
The dynamic behavior of the vapor flow in heat pipes is investigated at startup and during operation...
Six Jet A fuels, with varying compositions, were tested for low temperature flowability in a 190-lit...
The Idaho National Laboratory (INL) contribution to the Nuclear Energy Research Initiative (NERI) pr...
This thesis describes an experimental investigation of the flame transfer function between flow dist...
The Remote Field Eddy Current (RFEC) technique is ideal for inspecting unpiggable pipelines because ...
This report covers a portion of an ongoing investigation of the durability of adhesives for the High...
A general purpose, three-dimensional computational fluid dynamics code named PHOENICS, developed by ...
This study has been conducted in a partial fulfillment of a master of science degree in nuclear engi...
The purpose of the STME Main Injector Program was to enhance the technology base for the large-scale...
A millimeter-wave traveling wave tube (TWT) was developed using a dispersive, high-impedance forward...
An experimental and computational study was conducted on a high-speed, single-expansion-ramp nozzle ...
Recent work has been done with the goal of establishing ultralow emission aircraft gas turbine combu...
The design and development of an airborne flight-test experiment to study nonreacting gas jets injec...
The purpose of this study is to examine the predictive capabilities of fire models using the results...
A comparative study of wall mounted swept ramp injectors fitted with injector nozzles of different s...
The dynamic behavior of the vapor flow in heat pipes is investigated at startup and during operation...
Six Jet A fuels, with varying compositions, were tested for low temperature flowability in a 190-lit...
The Idaho National Laboratory (INL) contribution to the Nuclear Energy Research Initiative (NERI) pr...
This thesis describes an experimental investigation of the flame transfer function between flow dist...
The Remote Field Eddy Current (RFEC) technique is ideal for inspecting unpiggable pipelines because ...
This report covers a portion of an ongoing investigation of the durability of adhesives for the High...
A general purpose, three-dimensional computational fluid dynamics code named PHOENICS, developed by ...
This study has been conducted in a partial fulfillment of a master of science degree in nuclear engi...
The purpose of the STME Main Injector Program was to enhance the technology base for the large-scale...
A millimeter-wave traveling wave tube (TWT) was developed using a dispersive, high-impedance forward...