The flows observed in rocket engine turbopump inducers are characterized by complex, three-dimensional, unsteady, two phase structures, which con lead to strong forces acting on the pump components. We intend in this paper to present undergoing works performed at Snecma Moteurs - Rocket Engine Division, to progress in the control of these unsteady phenomena.
La Houille Blanche
Volume 87, 2001 - Issue 3-4
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