Cylinders are considered bluff bodies because at large Reynolds numbers the drag is dominated by the pressure losses in the wake.
(a) At point A the flow is laminar and drag is mainly due to the friction drag between the surface and the fluid. This friction is associated with the development of boundary layers and it scales with the Reynolds number. So, as the speed of the flow increases, Reynolds number increases and the friction drag decreases as the boundary layer helps in the smooth movement of the above layers.
(b) At point E, the flow changes from laminar to turbulent. At a Reynolds number between 10^5 and 10^6, the drag coefficient takes a sudden dip. The size of the wake decreases, indicating that the boundary layer separation on the cylinder occurs further along the surface than before. The phenomenon is related to the differences between laminar and turbulent boundary layer. The boundary layer and it's interaction with the local pressure gradient plays a major role in affecting the flow over a cylinder. In particular near the shoulder, pressure gradient changes from being negative (decreasing pressure) to positive (increasing pressure). The force due to pressure differences changes sign from being an accelerating force to being a retarding force. In response, the flow slows down. However, the fluid in the boundary layer has already given up some momentum because of viscous losses and viscous friction, and it does not have enough momentum to overcome the retarding force. Some fluid near the wall actually reverses direction, and the flow separates.
QUESTION 3 (14 marks) Variation in drag cylinder is shown in Figure 2 (a) At point coefficient (C...
could you please make clear answer? 5. Flow over a Bod;y (a) The drag coefficient for a smooth sphere is shown in the figure below. Determine the speed at the critical Re for a 42 mm diameter sphere in air. (This is a golf ball sized object.) You may assume air at 60°F. 0.5 0.4 0.3 0.2 0.1 4 105 Re-Du/v 103 106 107 (b) Ģolthal, "dimples" cause the drag drop to occur at a lower Reynolds number. The table...
Question 3-Concept Questions (10 points) a) What is the reason for having surface dimples (roughness) on a golf ball? Explain in 2-3 sentences. b) Draw the variation of lift and drag coefficients for a subsonic airfoil (at high Re number) over a Mach number range of 0.1-1.1. Explain the reason for trends Specify the primary drag mechanism for the following shapes in airstream at different Mach c) numbers. a. Symmetrical airfoil at an angle of attack of 4 degrees at...
please help Question 1 1.1 If the velocity distribution of a fluid flowing over a 1m² flat plate is given by u=l+ y + y, find the m. Assume dynamic viscosity to be y=6x10*(Ns/m”). force acting on a plate at y = [5 marks] 1.2 A 2D velocity field in an incompressible flow was measured by PIV method and determined to follow the following functions u= 2x’ +2y and v=x - 4y. Check whether your measurements are correct at a...
QUESTION 2 (14 marks) Explain how to form a steady uniform flow around a cylinder based on superposition (6 marks) (a) of several basic potential flows. (b) Based on the surface pressure distribution of the flow around the cylinder in (a) explain why the theoretical pressure distribution as illustrated in Fig. 1 is different (8 marks) from the corresponding experimental results. 3 Experimental Theoretical (inviscid) -3 0 30 60 90 120 150 180 β (deg) Figure 1 QUESTION 2 (14...
please draw and solve show every thing details “” Question 3 128 Marks 2 rectangular beam shown in the figure is subjected to a fluctuating axial force. It fluctuates between 5 kN and 15 kN keeping its direction. The beam is to be machined to the dimensions shown in the figure with a transvers hole of diameter d-14 mm/ Material of the beam is AISI 1040 CD steel (S-590 stress concentration factor as 2.2. K Pa, Sy 490 MPa). Take...
x=3 Question 3. A crank shaft mechanism is shown in Figure 3. Link Bis rotating with a constant angular velocity wgaz in the fixed reference frame A as shown in the figure. For this mechanism: (a) Using the vector kinematic equations and methods taught in this [20 marks] module, obtain the expressions for velocity and acceleration of point in the fixed frame A, in terms of wg.ls.c. and e. (b) Velocity analysis using MATLAB: As link B undergoes one full...
Question 2 Consider the system shown in Figure Q2, where Wis a unit step disturbance and R is a unit step input. 0.4 s+ 1 10 Figure Q2 (5 marks) (3 marks) (c) Find the value for K so that the steady state error due to w(t) is less than 0.01; 6 marks) (d) In order to eliminate the steady state error, show whether a PI controller can be successful 6 marks) (a) Find the expression of E(s)-R(s)-Y(s) in terms...
Question 2 Consider the system shown in Figure Q2, where Wis a unit step disturbance and R is a unit step input. 0.4 s+ 1 10 Figure Q2 (5 marks) (3 marks) (c) Find the value for K so that the steady state error due to w(t) is less than 0.01; 6 marks) (d) In order to eliminate the steady state error, show whether a PI controller can be successful 6 marks) (a) Find the expression of E(s)-R(s)-Y(s) in terms...
Question 1 [40 Points] Liquid mercury at 300 K flows over a flat surface at a free stream velocity 0.15 m/s. The flat plate is smooth with a width of 0.25 m and length 0.5 m and is kept at a uniform temperature of 400 K. The flow is parallel to the longer dimension of the plate. Find out: 1. MINIMUM LOCAL convective heat flux, q min and its location (60%) 2. Total convective heat transfer rate, q (40%) Use...
Question 3 A 10 m square and 7.5 m deep pit is to be excavated in a soil with a unit weight of 20 kN/m2. What is the stress relief at 2 m. 5 m and 10 m below the centre point of the bottom of the excavation? b. The circular flexible area is uniformly loaded (q 320 kN/m2). Determine the change in vertical stress: i. at point A At a point 2 m below point A 4 m A...