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.
Ribbed Coolant Liners for Combustion Chambers
NASA Tech Briefs ; 8 , 2
01.11.1984
Sonstige
Keine Angabe
Englisch
FLOW INVESTIGATION IN A TWO-PASS COOLANT CHANNEL WITH/WITHOUT RIBBED WALLS
British Library Conference Proceedings | 2003
|