Browse TRAIL Inventories

Investigation of transient combustion characteristics in a single tubular combustor

Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles

Effect of fuel nozzle protrusion on transient and steady-state turbojet combustor performance

Performance at High Temperatures and Pressures of an Annular Turbojet Combustor Having Articulated Liner Walls


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