3. (4 pts) Write down the velocity potential for a lifting circular cylinder in a uniform...
1. The lift on a spinning circular cylinder in a freestream with a velocity of 33.5 m/s and at standard sea level conditions is 6.3 N/m of span. Calculate the circulation around the cylinder. Enter your answer to two decimal places in units of m 2 /s. 2. In the given figure of flow over a cylinder, where is a stagnation point located? (R, pi/4) (R, pi/2) (R, pi) (R, 3*pi/2)
Advanced Fluid Mechanics Determine the streamfunction and velocity potential for uniform flow of strength U over a point source and sink of equal strength, m, located on the x-axis at +/-b (the source is at-b with the sink at +b, where b is not small). Write expressions for the u and v velocity components, and draw streamlines of the flow. Determine the location(s) of any and all stagnation points. Determine the streamfunction and velocity potential for uniform flow of strength...
Construct expressions for the stream function and velocity potential of flow around a circular cylinder. This is a source and a sink in a uniform stream, separated by a fixed distance. 1. Visualize the Flow Net (the streamlines and velocity potential lines) 2. Determine an expression for the velocity field. Note that the book uses cylindrical coordinates here Construct expressions for the stream function and velocity potential of flow around a circular cylinder. This is a source and a sink...
QUESTION 2 In an experiment to measure approaching uniform flow, U.to a non-rotating circular cylinder as shown in Figure Q2, a small hole is to be drilled at the stagnation point on the cylinder surface. (a) Determine the location of the drilled hole on the cylinder surface using potential flow theory by combining a doublet with a uniform flow. (3.5 marks) (b) Determine the theoretical pressure distribution expression on the cylinder surface, Pc and plot or sketch a graph of...
Problem 3: ter with density #1000k/m3 is flowing around a cylinder submergedinto a river. The river velocity is given by U-5 m/s and the cylinder radius is R -1.5 m. Calculate the pressure difference between point So (stagnation point) and the point S located at 45° on the surface. Note that as per the inviscid potential flow theory, the velocity at the external surface of the cylinder is given by v,--2U sin . Use g 9.81 m/s2 for gravity U...
Consider a circular cylinder of radius a whose central axis is stationary. The cylinder is surrounded by a fluid that is moving with a uniform steady velocity Uk far from the cylinder; the cylinder axis is in the z-direction The cylinder is also spinning on its axis with constant angular velocity, Ω2, where x, у and z are the usual Cartesian unit vectors We wish to model this 2D flow using an inviscid approximation. This is achieved by first calculating...
Name: Problem 4 (20 pts). The velocity potential for a cylinder rotating in a uniform stream of fluid is 2TT where U, a, Г are constants. The density of the flow is , and gravitational force is negligible. Compute the pressure difference between points A and B. -+ Name: Problem 4 (20 pts). The velocity potential for a cylinder rotating in a uniform stream of fluid is 2TT where U, a, Г are constants. The density of the flow is...
4. Uniformly moving point charge A point charge q is in uniform motion with velocity v = vzˆ, where v is a constant. At time t = 0 the charge is located at the origin. At a later time t 0 , at the field point x = x0, y = z = 0: (a) Find the scalar and vector potential. (b) What coordinate components does the electric field have? (c) What coordinate components does the magnetic field have? (d)...
Question 3 4-73 Solution For a given velocity field we are to calculate the vorticity Analysis The velocity field is V = (u, v, w)-(3.0+ 2.Ox-y)--(2.0-2.01.) j+10.5ryk Question 4 4-97 Solution For a given velocity field we are to determine if the flow is rotational or irrotational. 1 The flow is steady. 2 The flow is two-dimensional in the r-eplane. The velocity components for flow over a circular cylinder of radiur are Assumptions Analysis 11,--r sin θ| 1 +
3. Show that the velocity field with components (in spherical coordinates) K,-(4kr-3-2)cosa, pa-(2kr-3 +2)sin θ, ν, 0, k > 0,0 is a possible fluid velocity for an incompressible flow. For k 4, determine the stagnation points of the flow, if any. Hint: For stagnation point (W.,Vo,V)-(0,0,0) @s 2 3. Show that the velocity field with components (in spherical coordinates) K,-(4kr-3-2)cosa, pa-(2kr-3 +2)sin θ, ν, 0, k > 0,0 is a possible fluid velocity for an incompressible flow. For k 4,...