Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump

Figure 4

(a) Analytical results of the real part, 𝜔_𝑅, showing trend analyses on 𝐾 (𝑀𝜌Ω=0.035, 𝐾_drag=0). (b) Analytical results of imaginary part, 𝜔_𝐼, showing trend analyses on 𝐾 (𝑀𝜌Ω=0.035, 𝐾_drag=0).

(a)

(b)