consider the purely subsonic flow in a convergentdivergent duct the inlet throat and exit area a

Name: consider the purely subsonic flow in a convergentdivergent duct the inlet throat and exit area are 090 m2 060 m2 and 075 m2 respectively if the inlet mach number and pressure are 04 and 7000 35777
Uploaded: 2022-10-10T13:39:39-08:00
Duration: 2 min 33 s
Channel: Adi S
Description: consider the purely subsonic flow in a convergentdivergent duct the inlet throat and exit area are 090 m2 060 m2 and 075 m2 respectively if the inlet mach number and pressure are 04 and 7000 35777

Question

Adi S · Accepted Answer

Since M is equals to 1, add thrott, A is equals to A star, A T is equals to A star. So A .E upon

Question

Consider the purely subsonic flow in a convergent-divergent duct. The inlet, throat, and exit area are 0.90 m^2, 0.60 m^2, and 0.75 m^2, respectively. If the inlet Mach number and pressure are 0.4 and 7000 N/m^2, respectively, calculate M and p at the exit.

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