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The flow of air near the Earth’s surface is affected both by the wind and thermal currents. In certain circumstances the velocity field can be represented by
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Fox And Mcdonald's Introduction To Fluid Mechanics
- u=4x^2 and v=4y^2 a velocity field,what is magnitude of acceleration at (5,1) in m/s^2arrow_forwardSolve correctly please,please show all workarrow_forwardHome Work (steady continuity equation at a point for incompressible fluid flow: 1- The x component of velocity in a steady, incompressible flow field in the xy plane is u= (A /x), where A-2m s, and x is measured in meters. Find the simplest y component of velocity for this flow field. 2- The velocity components for an incompressible steady flow field are u= (A x* +z) and v=B (xy + yz). Determine the z component of velocity for steady flow. 3- The x component of velocity for a flow field is given as u = Ax²y2 where A = 0.3 ms and x and y are in meters. Determine the y component of velocity for a steady incompressible flow. Assume incompressible steady two dimension flowarrow_forward
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- The laminar flow of a fluid with a constant viscosity, 4, inside a channel is governed by the following boundary value problem (strong form): d'u dp for y E (0, h) "dy dr u = 0 at y = 0 and y = h vhere u is the fluid velocity and is the pressure drop in the direction of the flow. a) Derive the weak form of the boundary value problem described above.arrow_forwardExample 10.4-1 Stream Functions for a Flow Field The velocity components for a flow field are as follows: v, = a(x² – y²³), v, =-2axy V. V. %3D Prove that it satisfies continuity equation for two dimensional flows and find y. Plot streamlines for y=1 to y=6.arrow_forwardIn a stream of glycerine in motion, at a certain point the velocity gradient is 0.25 meter per sec per meter. The mass density of fluid is 1268.4 kg per cubic meter and kinematic viscosity is 6.30 x 10^-4 square meter per second. Calculate the shear stress in Pascal at the point.arrow_forward
- 1. A fluid is flowing steadily through a vertical tube of length L and radius R. It has constant density and viscosity. Pressure at the tube entrance and exit are Po and PL .Take appropriate assumption and coordinate system and write the differential equations to solve the flow field. Also state the boundary conditions that are applicable here. Po P.arrow_forward6. Problem We want to know the velocity component of a fluid flow normal to a given surface: v, = v"n. Compute the normal velocity u, for the following normal vector and flow vector. ) --E- 3.0 v = m/s V3 1.0arrow_forwardConsider the flow of a fluid between point 1 and 2. Compute the direction of flow, whether the fluid flows from point 1 to 2 or 2 to 1. Point 2 Point 1 The properties are listed below: Point 1: Pump Pressure = 1.25 x 105 Pa, Cross-sectional area - 15 x 104 m², Fluid velocity = 1 m/s Point 2: Pressure = 1.05 x 10³ Pa, Cross-sectional area = 5 x 104 m² Elevation above point 1-3m Other data: 3 m Density of fluid = 1000 kg/m³ Power delivered by the pump = 7.5 W (Assume efficiency = 100%)arrow_forward
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