I need the answer as soon as possible A large tank supplies helium through a converging-diverging nozzle to theatmosphere. The Pressure in the tank remains constant at 8.00 MPa and temperatureremains constant at 1000 K. Thereareshock waves in the nozzle.noThe nozzle is designed to discharge at an exit Mach number of 3.5. The exit area of thenozzle is 100 mm. Note that for helium, the specific heat ratio (k) is 1.66 and the ideal gasconstant (R) is 2077 J/kg-K.(a) Determine the pressure at the exit of the nozzle. (b) Determine the mass flow ratethrough the nozzle. (c) Sketch the pressure and Mach number behaviors for thisflow along the nozzle.n from a re ervo maainteined at 25 °Candihrongh a nozpressure

Nozzle : Nozzle is a duct or a pipe which controls the flow of fluid. Generally it is of two types…

A large tank supplies helium through a converging-diverging nozzle l8 atmosphere. The Pressure in the tank remains constant at 8.00 MPa 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 Ac nozzle is 100 mm. Note that for helium, the specific heat ratio (k) is 1.66 and the ideal gas constant (R) is 2077 J/kg-K. (a) Determine the pressure at the exit of the nozzle. (b) Determine the mass flow rate through the nozzle. (c) Sketch the pressure and Mach number behaviors for this flow along the nozzle. ined at 25 °Cand hrough a noZ7

A large tank supplies helium through a converging-diverging nozzle l8 atmosphere. The Pressure in the tank remains constant at 8.00 MPa 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 Ac nozzle is 100 mm. Note that for helium, the specific heat ratio (k) is 1.66 and the ideal gas constant (R) is 2077 J/kg-K. (a) Determine the pressure at the exit of the nozzle. (b) Determine the mass flow rate through the nozzle. (c) Sketch the pressure and Mach number behaviors for this flow along the nozzle. ined at 25 °Cand hrough a noZ7

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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