Help me please in Kaz daynimk. Q1: Air expands from a storage tank through a converging - diverging nozzle having athroat area of (70 cm). A normal shock occurs in the diverging part of the nozzle at alocation where the area is equal to twice the throat area, with the exit area of the nozzleequal to three times the throat arca. Assuming isentropic flow except through the shockand that the storage tank pressure and temperature are (250 kpa and 77 °c).Determine:1- The Mach number and stagnation pressure at the nozzle exit plane.2- Exit plane pressure and velocity.3- The ratio of the exit to shock areas (A/A).

Given:The throat area is .The shock area is .The exit area is .The pressure and temperature is and…

Q1: Air expands from a storage tank through a converging diverging nozzle having a hroat area of (70 cm). A normal shock occurs in the diverging part of the nozzle at a location where the area is equal to twice the throat area, with the exit area of the nozzle equal to three times the throat area. Assuming isentropic flow except through the shock and that the storage tank pressure and temperature are (250 kpa and 77 °c). Determine: 1- The Mach number and stagnation pressure at the nozzle exit plane. 2- Exit plane pressure and velocity. 3- The ratio of the exit to shock areas (A/A).

Q1: Air expands from a storage tank through a converging diverging nozzle having a hroat area of (70 cm). A normal shock occurs in the diverging part of the nozzle at a location where the area is equal to twice the throat area, with the exit area of the nozzle equal to three times the throat area. Assuming isentropic flow except through the shock and that the storage tank pressure and temperature are (250 kpa and 77 °c). Determine: 1- The Mach number and stagnation pressure at the nozzle exit plane. 2- Exit plane pressure and velocity. 3- The ratio of the exit to shock areas (A/A).

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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