A hovercraft weighs M 1500 kg and hovers without changing altitude. The exit flow exhausts to atmospheric pressure at sea-level. The flow is steady, incompressible and uniform properties can be assumed on all control surfaces. Assume air density = 1.22 kg/m'. In your solution, write all equations using variables names. Only plug in numerical values in part d).

A hovercraft weighs M 1500 kg and hovers without changing altitude. The exit flow exhausts to atmospheric pressure at sea-level. The flow is steady, incompressible and uniform properties can be assumed on all control surfaces. Assume air density = 1.22 kg/m'. In your solution, write all equations using variables names. Only plug in numerical values in part d).

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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