Consider a flow through a nozzle, as shown in the figure below: P"Pm - 50 mis 4- 0.02 m² Streamline A, = 0.2 m Ą = The air flow is steady, incompressible and inviscid. The density of air is 1.23 kg/m². The pressure difference (p, - Pam) is kPa (round off to the nearest integer).

Consider a flow through a nozzle, as shown in the figure below: P"Pm - 50 mis 4- 0.02 m² Streamline A, = 0.2 m Ą = The air flow is steady, incompressible and inviscid. The density of air is 1.23 kg/m². The pressure difference (p, - Pam) is kPa (round off to the nearest integer).

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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Question

Consider a flow through a nozzle, as shown in the figure below:
2
Pi
P2= Pam
Streamline
V = 50 mis
A, = 0.2 m
A = 0.02 m
The air flow is steady, incompressible and inviscid. The density of air is 1.23 kg/m².
The pressure difference (p, - Pam) is
kPa (round off to the nearest integer).

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