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Numerical Modeling of Regenerative Cooling System for Large Expansion Ratio Rocket Engines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In this study, the performance of regenerative cooling system for large expansion ratio rocket engines (Ae/At ∼ 100) is investigated numerically. During combustion and gas expansion, the walls of the combustion chamber ...
Traversing Hot Jet Ignition in a Constant Volume Combustor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Hotjet ignition of a combustible mixture has application in internal combustion engines, detonation initiation, and wave rotor combustion. Numerical predictions are made for ignition of combustible mixtures using a traversing ...
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