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Comparative Numerical Study of Film Cooling Strategies for Thermal Protection of a Kerosene-Fueled Oblique Detonation Combustor
Thermal protection remains a major challenge for oblique detonation engines (ODEs), whose combustors combine intense heat release, anchored on oblique detonation waves (ODWs). This study numerically investigates the effects of coolant type and mass flow rate on the flow structure, thermal environmen
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