Air is driven from a reservoir at 1.3 MPa through a converging-diverging nozzle with a design Mach number of 2.5. Determine the exit Mach number (to two significant figures) when the back pressure is: a) 10.0 kPa; b) Equal to the back pressure required to sustain a normal shock at the exit plane. 610.7 kPa. d) 966.3 kPa; and 1270.0 kPa.

Elements Of Electromagnetics
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I want part d and e

Air is driven from a reservoir at 1.3 MPa through a converging-diverging nozzle with a design Mach
number of 2.5. Determine the exit Mach number (to two significant figures) when the back pressure is:
a)
10.0 kPa;
b)
Equal to the back pressure required to sustain a normal shock at the
exit plane.
c)
610.7 kPa.
d)
966.3 kPa; and
e)
1270.0 kPa.
Transcribed Image Text:Air is driven from a reservoir at 1.3 MPa through a converging-diverging nozzle with a design Mach number of 2.5. Determine the exit Mach number (to two significant figures) when the back pressure is: a) 10.0 kPa; b) Equal to the back pressure required to sustain a normal shock at the exit plane. c) 610.7 kPa. d) 966.3 kPa; and e) 1270.0 kPa.
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