Question
A round thin disk of radius $R$ is oriented perpendicular to a fluid stream. The pressure distributions on the front and back surfaces are measured and presented in the form of pressure coefficients. The data are modeled with the following expressions for the front and back surfaces, respectively: $$\begin{array}{ll}\text { Front Surface } & C_{p}=1-\left(\frac{r}{R}\right)^{6} \\\text { Rear Surface } & C_{p}=-0.42\end{array}$$Calculate the drag coefficient for the disk.
Step 1
Step 1: The drag coefficient $C_D$ is given by the formula: $$C_D = \frac{F_D}{\frac{1}{2}\rho U^2 A}$$ where $F_D$ is the drag force, $\rho$ is the fluid density, $U$ is the fluid velocity, and $A$ is the area of the disk. Show more…
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In an experiment to determine drag, a circular cylinder of diameter $d$ was immersed in a steady two-dimensional incompressible flow. Measurements of velocity and pressure were made at the boundaries of the control surface shown. The pressure was found to be uniform over the entire control surface. The $x$ component of velocity at the control surface boundary was approximately as indicated by Fig. P5.63. From the measured data, calculate the drag force per unit length of the cylinder, based on diameter $d$ and the free stream dynamic head $\left(1 / 2 \rho V_{\infty}^{2}\right)$.
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