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Influence of the Blade Number on Inducer Cavitating Behavior

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Academic year: 2021

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Figure

Fig. 1 Rocket engine turbopump inducer
Fig. 4 Scheme of the inducer test section including the acquisition equipmentFig. 3General view of the LML large test facility
Fig. 8 Torque coefficient drop for IND3 and IND5 (N ref , Q n , type
Fig. 11 Influence of the rotation speed on the value of s corre- corre-sponding to (a) 3% W 1 drop and (b) 3% v 1 drop (Q n , type #2 experiments)
+5

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