Research Article

Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump

Figure 2

(a) FFT analyses of pressure fluctuation at inlet of the turbopump. (b) Analytical result by inertia model and experimental result of pressure fluctuation at inlet of turbopump. (The size of the bubbles indicate the amplitude of the pressure fluctuation).
717013.fig.002a
(a)
717013.fig.002b
(b)