Consider the lifting flow over a circular cylinder. The lift coefficient is 7. Calculate the peak coefficient of pressure.
Consider the lifting flow over a circular cylinder. The lift coefficient is 7. Calculate the peak coefficient of pressure.
Maximum velocity for lifting flow over a circular cylinder occurs at top surfaces and is equal to summation of non-lifting value of maximum flow velocity, – 2{V_\infty } and vortex \frac{{ – \tau }}{{2\pi R}} therefore,V = – 2{V_\infty } – \frac{\tau }{{2\pi R}}coefficient of lift is {c_l} = \frac{\tau }{{R{V_\infty }}} = 7therefore, \frac{\tau }{R} = 7{V_\infty }; On substitution the value of \frac{\tau }{R} in the velocity equation, we get V = – 2{V_\infty } – \frac{7}{{2\pi }}{V_\infty } = – 3.11{V_\infty }therefore peak coefficient of pressure will be {C_p} = 1 – {\left( {\frac{V}{{{V_\infty }}}} \right)^2} = 1 – {\left( { – \frac{{3.11{V_\infty }}}{{{V_\infty }}}} \right)^2} = 1 – {\left( { – 3.11} \right)^2} = – 8.67