A static thrust stands as it showed in the Figure. The intake velocity is 200 m/s, exhaust velocity is 500 m/s, intake cross-section area 1 m, intake pressure is -22.5 kPa, and exhaust pressure is pressure and considered zero. Determine the anchoring force (Fth).( Density = 1.02kg / (m ^ 3)) —'y'dControl volume+M A static thrust stands as it showed in the Figure. The intake velocity is 200m/s, exhaust velocity is 500 m/s, intake cross-section area = 1 m², intakepressure is -22.5 kPa, and exhaust pressure is atmospheric pressure andconsidered zero. Determine the anchoring force (F). (p=1.02 kg/m³)TRENER11Control volumeJ

Given data:- The intake velocity = 200 m/s, exhaust velocity=500 m/s, intake cross-section area =1…

Answered: A static thrust stands as it showed in…

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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A static thrust stands as it showed in the Figure. The intake velocity is 200 m/s, exhaust velocity is 500 m/s, intake cross-section area 1 m, intake pressure is -22.5 kPa, and exhaust pressure is pressure and considered zero. Determine the anchoring force (Fth).( Density = 1.02kg / (m ^ 3))

A static thrust stands as it showed in the Figure. The intake velocity is 200
m/s, exhaust velocity is 500 m/s, intake cross-section area = 1 m², intake
pressure is -22.5 kPa, and exhaust pressure is atmospheric pressure and
considered zero. Determine the anchoring force (F). (p=1.02 kg/m³)
TRENER
11
Control volume
J

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