NASA NTRS · 19830000696
Ribbed Coolant Liners for Combustion Chambers
Abstract
Coolant-carrying liner for combustion chambers runs cooler and tolerates high-temperature excursions without burning out. Hot gases flowing through core prevented by liner from damaging shell. Concept applicable to such high-temperature chambers as rocket pre-burners, turbojet cans, stationary-turbine combustors, oil burners, and high-pressure chemical reactors.
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Wagner, W. R.. 1984-11-01. Ribbed Coolant Liners for Combustion Chambers. https://ntrs.nasa.gov/citations/19830000696
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