Ignition and chemical kinetics in hypersonic ramjets
Explore the source record for details and available documents.
Engineering topics
Publications and source records attributed to Lezberg, E. A..
Explore the source record for details and available documents.
Explore the source record for details and available documents.
High temperature synthetic air heater for use with hypersonic tunnel
Comparison of hydroxyl profiles with kinetic calculations - spectral line absorption of combustion products of hydrogen and preheated air
Hydroxyl radical concentration measurement from spectral line absorption in supersonic nozzle flow of hydrogen-air combustion products
Temperature measurements in supersonic nozzles for hydrogen-air and methane-air combustion products at stagnation temperatures up to 5,400 degrees rankine and pressures up to 4.5 atmospheres
Exhaust nozzle recombination for hydrogen-fueled subsonic combustion ramjet engines
Effect of exhaust nozzle recombination on hypersonic ramjet performance
Effect of exhaust nozzle recombination on hypersonic ramjet performance
Temperature measurements in supersonic nozzles for hydrogen-air and methane-air combustion products at stagnation temperatures up to 5400 degrees rankine and pressures up to 4.5 atmospheres
Exhaust nozzle recombination for hydrogen-fueled subsonic combustion ramjet engines
Exhaust nozzle recombination of hydrogen fuel in subsonic ramjet engines at hypersonic speeds
Large quantities of high-temperature air are needed for work with hypersonic flight problems. At temperatures above 2500 degrees Reamur, where conventional heat exchangers have exceeded their material limits, regenerative pebble-bed exchangers may be used with high-temperature refractories. The design of such a heat exchanger requires the use of reliable heat-transfer coefficients for a packed bed. Considerable data are available on the subject, but they spread over two orders of magnitude at any one Reynolds number value. The facility from which the present data were obtained is used at the Lewis Research Center (NASA) for testing air-breathing engine components. The purpose of this work was to obtain heat-transfer data during the initial operation of the bed as a guide to the design of similar equipment. The facility was designed with a conservative estimate of the heat-transfer coefficient, and is shown schematically. Temperatures throughout the packing were measured continuously so that point values of the coefficient might be obtained.