Consider again the two-tank system in Fig. 6.13. Assume that only nozzle A is present and that it is a convergent divergent nozzle of exit-to-throat area ratio 2 with the same throat diameter as before. Sketch the variation of the exit pressure,mass flow rate, exitMach number, and the ambient pressure of nozzle A with time starting from time 0+ until steady state is reached. Although the profiles can be qualitative, key instants should be marked with numerical values for these quantities. The pressure profiles must be shown together in the same figure using the same axes.

Transcribed Image Text:

1 MPa A B 0.1 MPa Throat Throat Fig. 6.13 Illustration of Nozzle-Nozzle interaction (Adapted from White)