Exploratory performance investigation of co-burner-type combustors
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Metzler, Allen J↗
Engineering topics
Metzler, Allen J
Publications and source records attributed to Metzler, Allen J.
Simulated afterburner performance with hydrogen peroxide injection for thrust augmentation
Combustion performance of three afterburner configurations was evaluated at simulated altitude flight conditions with liquid augmentation to the primary combustor. Afterburner combustion efficiency and stability were better with injection of high-strength hydrogen peroxide than with no injection or with water injection. Improvements were observed in afterburner configurations with and without flameholders and in a short-length afterburner. At a peroxide-air ratio of 0.3, combustion was stable and 85 to 90 percent efficient in all configurations tested. Calculated augmented net-thrust ratios for peroxide injection with afterburning were approximately 60 percent greater than those for water injection.
Metzler, Allen J↗
Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation
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Metzler, Allen J↗
Low-pressure performance of experimental prevaporizing tubular combustor using approximately stoichiometric admission of fuel-air mixture into the primary zone
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Hibbard, Robert R↗
Minimum spark-ignition energies of 12 pure fuels at atmospheric and reduced pressure
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Metzler, Allen J↗
Minimum Ignition of Six Pure Hydrocarbon Fuels of the C2 and C6 Series
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Metzler, Allen J↗
Combustion efficiencies in hydrocarbon-air systems at reduced pressures
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Hibbard, Robert R↗