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<p>The overall  of a real square flat plate perpendicular to the flow is often given as 1.17. Flow patterns and therefore  for some shapes can change with the Reynolds number and the roughness of the surfaces.</p>

<p><big> Drag coefficient examples </big></p>
<p><big> General </big></p>
<p>In general,  is not an absolute constant for a given body shape. It varies with the speed of airflow (or more generally with <a href="page.php?w=Reynolds_number">Reynolds number</a> ). A smooth sphere, for example, has a  that varies from high values for <a href="page.php?w=laminar_flow">laminar flow</a></p><p>
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