HAL (France)
open access
Non-linear longitudinal combustion instabilities in a sub- and supercritical liquid rocket combustor
Future liquid rocket engines tasked to propel space launchers are expected to satisfy new industry needs. Chiefly among them, reusability. Vertically landing a rocket stage requires re-lightable and high-performance engines, capable of working across wide ranges of thrust. Such deep-throttlable engi
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