A large tank supplies helium through a converging-diverging nozzle to the atmosphere. Pressure in the tank remains constant at 8.00 MPa (abs) and temperature remains constant at 1000 K. There are no shock waves in the nozzle. The nozzle is designed to discharge at an exit Mach number of 3.5. The exit area of the nozzle is 100 mm². Determine the mass flow rate through the device. For helium: specific heat ratio k = 1.66; ideal gas constant R = 2077 J/kg.K. To = 1000 K Po= 8 MPa (abs) Throat Helium A₁ = 100 mm² Ma₁ = 3.5

A large tank supplies helium through a converging-diverging nozzle to the atmosphere. Pressure in the tank remains constant at 8.00 MPa (abs) and temperature remains constant at 1000 K. There are no shock waves in the nozzle. The nozzle is designed to discharge at an exit Mach number of 3.5. The exit area of the nozzle is 100 mm². Determine the mass flow rate through the device. For helium: specific heat ratio k = 1.66; ideal gas constant R = 2077 J/kg.K. To = 1000 K Po= 8 MPa (abs) Throat Helium A₁ = 100 mm² Ma₁ = 3.5

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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