Devaraj van der Meer, Gerrit de Bruin, November 2, 2006 Exam Advanced Fluid Mechanics (357001) November 3, 2006 9:00 – 12:30 This exam is an ‘open book’ exam, i.e., you can use your course book, lecture notes and your own notes in solving the problems that constitute this exam. There are five problems of varying length and difficulty. The number of points that can maximally be earned by giving a correct answer is indicated at the end of each question. There are 100 points in total. Good luck ! Problem 1 – Outflow of a vertical pipe Water flows through a pipe in a gravitational field as shown in the accompanying figure. Neglect the effects of viscosity and surface tension. The velocity of the fluid at z = 0, where the water leaves the pipe, is uniform and has a magnitude u0. The cross-sectional area of the orifice is A0. a) Solve the appropriate conservation equations for the variation of the cross-sectional area of the fluid column A(z) after the water has left the pipe. [5 pts.] Problem 2 – Irrotational vortices Two two-dimensional irrotational vortices of strength Γ1 and Γ2 respectively interact with each other through their mutual velocity fields. The vortices are initially at a distance d from each other. In answering the first three questions (a, b1, and b2) exclude the special cases Γ1 = Γ2 and Γ1 = – Γ 2 . a) Argue that, at a distance very far away from the vortex pair, the flow field of the two vortices will look like that of a single vortex. Calculate the strength of this vortex. [5 pts.] b1) In the laboratory frame there must be a point in which the velocity field vanishes. Calculate the distances of the two vortices to this point in terms of Γ1, Γ2 and d. [6 pts.] b2) Describe the motion of the two vortices for the case that both vortices are corotating (i.e. in the same direction, e.g., Γ1 > 0 and Γ2 > 0) and for the case that they are counter-rotating (e.g., Γ1 > 0 and Γ2 < 0). [3 pts.] Now consider the special case: Γ1 = – Γ2 ≡ Γ, a so-called counter-rotating vortex pair. c1) Describe the motion of such a counter-rotating vortex pair as they approach a wall that is parallel to the line connecting the two vortices. [2 pts.] Exam Adv. Fluid Mech., Friday November 3, 2006, 9:00 – 12:00 page 1 of 3 Devaraj van der Meer, Gerrit de Bruin, November 2, 2006 c2) Calculate both components of the velocities of each of the vortices, i.e., both the component parallel to as the component perpendicular to the wall. In your calculation let s be the distance of the vortex pair to the wall. [6 pts.] d) Write down the equations of motion for each vortex and show that in the limit of d >> s they lead to the following equation of motion for the distance d between the vortices: 2 ∂ 2d Γ 1 = ∂t 2 π d 3 [6 pts.] (Remark: This equation can be solved analytically, from which the trajectory of the vortices can be calculated.) Problem 3 – Waves on a fluid-fluid interface Two immiscible inviscid fluids at rest are positioned on top of each other such that the upper halfspace z > 0 is covered with fluid 1 with density ρ1 and the lower halfspace z < 0 with fluid 2 (density ρ2). The surface tension of the two-fluid interface is equal to σ. a) For a (small) disturbance η of the interface, give the dynamic boundary condition at the interface. Take its surface tension into account, and formulate the above boundary condition in terms of the flow potentials φ1 and φ2 of the fluids and the disturbance. [8 pts.] Using an ansatz for small disturbances of the interface of the form η ( x, t ) = ηˆ eik ( x −ct ) one can show that from the kinematic boundary conditions the potentials in the upper and lower fluid must satisfy: ϕ1 = icηˆ e− kz eik ( x−ct ) ; ϕ2 = −icηˆ ekz eik ( x−ct ) b) Show that the dynamic boundary condition of a) leads to the following relation: ρ − ρ2 g σk c2 = − 1 + ρ1 + ρ 2 k ρ1 + ρ 2 Carefully indicate the different approximations that you make and why they are valid [7 pts.] c) Determine the condition on k for which traveling waves are possible. Are traveling waves ever possible if ρ1 > ρ2 ? [7 pts.] Exam Adv. Fluid Mech., Friday November 3, 2006, 9:00 – 12:00 page 2 of 3 Devaraj van der Meer, Gerrit de Bruin, November 2, 2006 Problem 4 – Rotating sphere in a viscous fluid A rigid sphere of radius a is rotating with a constant angular velocity Ω in a fluid which is at rest at infinity. Assume that the Reynoldsnumber Re = a 2Ω ν ≪1 . is very small. This problem is conveniently treated in spherical polar coordinates where the axis of rotation coincides with the z-axis. a) Based on symmetry, argue that none of the flow variables u and p can depend on the azimuthal coordinate φ, most notably, the pressure gradient vanishes in this direction. Also argue that the only non-zero flow component is the one in azimuthal direction. [5 pts.] b) Show that, using the separation ansatz uϕ = f ( r )sin θ , the appropriate equation for the flow field leads to d 2 df r −2f =0 dr dr [8 pts.] c) Show that the general solution of the above equation is a linear combination of two terms of the form r n, and using the appropriate boundary conditions show that Ωa 3 uϕ = 2 sin θ r [7 pts.] d) Calculate the torque that the sphere exerts on the liquid. [7 pts.] Problem 5 – Perturbation expansion The temperature distribution in a certain flow problem is described by a differential equation, which in non-dimensional form and together with the boundary conditions is given by d2 3 (Y ) = ε Y ; with: Y (0) = 1 ; dx 2 dY dx =0 . x =1 (Here the parameter Y is the square root of the temperature Y = T . Knowledge of this fact is not necessary to solve the below problems.) a) Assuming that ε is a small parameter, solve this boundary value problem using a regular perturbation expansion up to 1st order in ε. [12 pts.] b1) If ε is very large (i.e., ε >> 1) one can try to reformulate the problem such that it can still be treated within the framework of a perturbation expansion in a small parameter. Give such an alternative formulation of the problem. [3 pts.] b2) State whether this alternative formulation is regular or singular and prove your statement. [3 pts.] Exam Adv. Fluid Mech., Friday November 3, 2006, 9:00 – 12:00 page 3 of 3