Drag coefficient: Difference between revisions

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<div class="definition"><div class="short_definition">A dimensionless ratio of the component of force parallel to the direction of flow  ([[drag]]) exerted on a body by a fluid to the [[kinetic energy]] of the fluid multiplied by a characteristic  surface area of the body.</div><br/> <div class="paragraph">In symbols, the drag coefficient ''C''<sub>''D''</sub> is  <div class="display-formula"><blockquote>[[File:ams2001glos-De46.gif|link=|center|ams2001glos-De46]]</blockquote></div> where &#x003c1; is the fluid [[density]], ''U'' the speed, and ''L'' a [[characteristic length]] of the body. [[Rayleigh's  formula]] expresses the drag coefficient as proportional to a power of the [[Reynolds number]] (Re),  <div class="display-formula"><blockquote>[[File:ams2001glos-De47.gif|link=|center|ams2001glos-De47]]</blockquote></div> For [[Couette flow]], ''n'' = &minus;1 and the constant is 2. In most [[aerodynamic]] experiments ''n'' lies between  &minus;1/4 and &minus;1/2. The drag coefficient for the force exerted by the [[atmosphere]] on the earth is  called the [[skin-friction coefficient]].</div><br/> </div>
<div class="definition"><div class="short_definition">A dimensionless ratio of the component of force parallel to the direction of flow  ([[drag]]) exerted on a body by a fluid to the [[kinetic energy]] of the fluid multiplied by a characteristic  surface area of the body.</div><br/> <div class="paragraph">In symbols, the drag coefficient ''C''<sub>''D''</sub> is  <div class="display-formula"><blockquote>[[File:ams2001glos-De46.gif|link=|center|ams2001glos-De46]]</blockquote></div> where &#x003c1; is the fluid [[density]], ''U'' the speed, and ''L'' a [[characteristic length]] of the body. [[Rayleigh's  formula]] expresses the drag coefficient as proportional to a power of the [[Reynolds number]] (Re),  <div class="display-formula"><blockquote>[[File:ams2001glos-De47.gif|link=|center|ams2001glos-De47]]</blockquote></div> For [[Couette flow]], ''n'' = -1 and the constant is 2. In most [[aerodynamic]] experiments ''n'' lies between  -1/4 and -1/2. The drag coefficient for the force exerted by the [[atmosphere]] on the earth is  called the [[skin-friction coefficient]].</div><br/> </div>
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Revision as of 14:05, 20 February 2012



drag coefficient

A dimensionless ratio of the component of force parallel to the direction of flow (drag) exerted on a body by a fluid to the kinetic energy of the fluid multiplied by a characteristic surface area of the body.

In symbols, the drag coefficient CD is
ams2001glos-De46
where ρ is the fluid density, U the speed, and L a characteristic length of the body. Rayleigh's formula expresses the drag coefficient as proportional to a power of the Reynolds number (Re),
ams2001glos-De47
For Couette flow, n = -1 and the constant is 2. In most aerodynamic experiments n lies between -1/4 and -1/2. The drag coefficient for the force exerted by the atmosphere on the earth is called the skin-friction coefficient.


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