resultant force vector acting on the body to be derived. Figure 2 shows a steady, uniform two-dimensional jet of liquid in the atmosphere impinging on a flat plate inclined at an angle q to the jet axis. The jet cross section area is A, and its velocity is u. The liquid density isr. It is assumed that there are no flow losses, and that all the streamlines end up parallel to the plate. Explain why the resultant force acts perpendicular to the plate, and show that its magnitude is: R 22. A.u cos? Figure 2

resultant force vector acting on the body to be derived. Figure 2 shows a steady, uniform two-dimensional jet of liquid in the atmosphere impinging on a flat plate inclined at an angle q to the jet axis. The jet cross section area is A, and its velocity is u. The liquid density isr. It is assumed that there are no flow losses, and that all the streamlines end up parallel to the plate. Explain why the resultant force acts perpendicular to the plate, and show that its magnitude is: R 22. A.u cos? Figure 2

Name: HYDRAULICS b) Uniform streams of fluid cross the boundary of a control
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Description: HYDRAULICS b) Uniform streams of fluid cross the boundary of a control volume containing asolid object. Briefly explain how Newton's 2nd and 3rd laws allow theresultant force vector acting on the body to be derived. Figure 2 shows asteady, uniform tw

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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