Consider the nonlifting flow over a circular cylinder of a given radius, where V_{\infty} = 20\; ft/s. If  V_{\infty} is doubled, that is, V_{\infty} = 40 ft/s, does the shape of the streamlines change? Explain.

Consider the nonlifting flow over a circular cylinder of a given radius, where V_{\infty} = 20 ft/s. If  V_{\infty} is doubled, that is, V_{\infty} = 40 ft/s, does the shape of the streamlines change? Explain.

Worldtech Asked on 4th November 2019 in Aerodynamics.
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    \frac{V_{r}}{V_{\infty}}=\left ( 1-\frac{R^{2}}{r^{2}} \right )cos\theta

    \frac{V_{\theta}}{V_{\infty}}=-\left ( 1+\frac{R^{2}}{r^{2}} \right )sin\theta

    At \left ( r,\theta \right ) ,V_{r} and V_{\infty} is proportional to V_{\infty}. Therefore \overrightarrow{V} is same  what V_{\infty}   may be. The shape of the streamlines will remain same it will not change.

    techAir Answered on 4th November 2019.
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