Solve the following fluid mechanics questions Consider a steady, incompressible, irrotational and inviscidflow past an airfoil. If the velocities at points 1 and 2 of theairfoil are U1= 101 m/s and U2= 71 m/s, respectively, whatis the pressure difference Ap = P2density of air is p=1.13 kg/m, and g=9.8 m/s?. Keep ONE– P1, in kPa? Thedecimal point in your answer.UoU2 The water in an 5.2 m-diameter, 6.6 m-high above-groundswimming pool is to be emptied by unplugging a 4.0 cm-diameter, 21.4 m-long horizontal pipe attached to thebottom of the pool. Determine the maximum discharge rateof water (m /s) through the pipe. g39.81 m/s2. Keep FOURdecimal points in your answer.

(Since two questions are submitted, as per policy only one (first) question is allowed to be…

Consider a steady, incompressible, irrotational and inviscid flow past an airfoil. If the velocities at points 1 and 2 of the airfoil are U1= 101 m/s and U2= 71 m/s, respectively, what is the pressure difference Ap = P2 – P1, in kPa? The density of air is p=1.13 kg/m2, and g=9.8 m/s2. Keep ONE decimal point in your answer. U1 Uo U2

Consider a steady, incompressible, irrotational and inviscid flow past an airfoil. If the velocities at points 1 and 2 of the airfoil are U1= 101 m/s and U2= 71 m/s, respectively, what is the pressure difference Ap = P2 – P1, in kPa? The density of air is p=1.13 kg/m2, and g=9.8 m/s2. Keep ONE decimal point in your answer. U1 Uo U2

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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