Problem (1) A large vacuum tank, held at 60kmabsolute. Suck sea-level standard air through aConverging Nozzle whose throat diameter is (3 cm).Estimate @ the mass flow rate through the Nozzleand the Mach No. at the throat. Assume theflow as an isentrapic flaw.

Given Data The pressure inside the tank is: P2=60 kPa The nozzle throat diameter is: d=3 cm=0.03 m…

Problem (1): A large vacuum tank, held at sokf -absolute. Suck, sea-level standard air through a Converging Nozzle whose thront diameter is (3 cm). Estimate @ the mass flow rate through the Nozzle and the Mach No. at the throat. Assume the flow as an isentrapic flow.

Problem (1): A large vacuum tank, held at sokf -absolute. Suck, sea-level standard air through a Converging Nozzle whose thront diameter is (3 cm). Estimate @ the mass flow rate through the Nozzle and the Mach No. at the throat. Assume the flow as an isentrapic flow.

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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Problem (1) A large vacuum tank, held at 60km
absolute. Suck sea-level standard air through a
Converging Nozzle whose throat diameter is (3 cm).
Estimate @ the mass flow rate through the Nozzle
and the Mach No. at the throat. Assume the
flow as an isentrapic flaw.

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