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What is Flame Stabilization in Scramjet Combustor about?

This study examines flame stabilization in a hydrogen-fueled scramjet combustor with a rear-wall-expansion cavity at Mach 2.92. It compares four fuel injection schemes, finding that two cascaded injectors (30 mm and 10 mm upstream) provide the most stable combustion and wider heat release zones. The research highlights the importance of injector configuration for effective flame stabilization in scramjet applications.

Author

Deeptankar Ghosh

Language

EN