The results of fuel-air ratio and temperature surveys made in the flame stabilizing zone of a 16-inch ram-jet combustor indicated that the distribution of combustible mixture immediately downstream of a flame holder should be mechanically controlled if a preferred mixture composition is to be maintained in that zone. A sloping-baffle combustor configuration gave combustion efficiencies of 90 percent or greater over a range of fuel-air ratios from 0.010 to 0.045
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
Effect of fuel distribution and flame stabilization techniques on combustion stability limits for sw...
A preliminary evaluation was made of three types of combustor con-figuration in a 48-inch-diameter r...
Results obtained with three different burner configurations in a connected-pipe investigation of a 1...
A preliminary evaluation was made of three types of combustor configurations in a 48-inch-diameter r...
Results of a theoretical and experimental study of the total pressure losses and combustion efficien...
The results of an altitude test-chamber investigation of the effects of a number of design changes a...
A ram-jet engine with an experimental 48-inch-diameter combustor was investigated in a free-jet faci...
Altitude-test-chamber investigation of effects of flame-holder blocked area and gutter width on perf...
An investigation of the altitude performance of a 20-inch-diameter high-temperature-ratio ram-jet co...
The effects of mass-flow ratio on the additive drag and normal-shock position of a single oblique-sh...
Free jet tests of 48 inch diameter ramjet combustor with annular can-type flame holde
The ram jet is basically one of the most dimple types of aircraft engine. It consists only of an inl...
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
The results of an analytical investigation of the theoretical air specific impulse performance and a...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
Effect of fuel distribution and flame stabilization techniques on combustion stability limits for sw...
A preliminary evaluation was made of three types of combustor con-figuration in a 48-inch-diameter r...
Results obtained with three different burner configurations in a connected-pipe investigation of a 1...
A preliminary evaluation was made of three types of combustor configurations in a 48-inch-diameter r...
Results of a theoretical and experimental study of the total pressure losses and combustion efficien...
The results of an altitude test-chamber investigation of the effects of a number of design changes a...
A ram-jet engine with an experimental 48-inch-diameter combustor was investigated in a free-jet faci...
Altitude-test-chamber investigation of effects of flame-holder blocked area and gutter width on perf...
An investigation of the altitude performance of a 20-inch-diameter high-temperature-ratio ram-jet co...
The effects of mass-flow ratio on the additive drag and normal-shock position of a single oblique-sh...
Free jet tests of 48 inch diameter ramjet combustor with annular can-type flame holde
The ram jet is basically one of the most dimple types of aircraft engine. It consists only of an inl...
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
The results of an analytical investigation of the theoretical air specific impulse performance and a...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
Effect of fuel distribution and flame stabilization techniques on combustion stability limits for sw...
A preliminary evaluation was made of three types of combustor con-figuration in a 48-inch-diameter r...