We want to create a converging nozzle. The nozzle will be connected to a shop compressed air system through a tank. The requirement for the nozzle inlet area is A₁ = 20 cm² and the requirement for the nozzle exit area is A₂ = 5 cm². We want to find the air tank pressure, inlet Mach number, and standard volume flow rate for the different exit Mach numbers listed below: (Assume air inside tank has negligible velocity, temperature of the air inside the tank is 288 Kelvin, the nozzle exhausts to standard conditions P = 101 kilopascals): (a) M₂ = 0.3 (b) Me = 0.5 (c) M₂ = 1.0 Note: the standard volume flow rate (Q = m/p) assumes the density of the air is standard with p = 1.23kg/m³

We want to create a converging nozzle. The nozzle will be connected to a shop compressed air system through a tank. The requirement for the nozzle inlet area is A₁ = 20 cm² and the requirement for the nozzle exit area is A₂ = 5 cm². We want to find the air tank pressure, inlet Mach number, and standard volume flow rate for the different exit Mach numbers listed below: (Assume air inside tank has negligible velocity, temperature of the air inside the tank is 288 Kelvin, the nozzle exhausts to standard conditions P = 101 kilopascals): (a) M₂ = 0.3 (b) Me = 0.5 (c) M₂ = 1.0 Note: the standard volume flow rate (Q = m/p) assumes the density of the air is standard with p = 1.23kg/m³

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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