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the equation for the drag force on the square paper is may be assumed to be is the form of \( F = \frac{1}{2} \rho v^{2} C_{D} A \)
where F is the aerodynamic drag force
\( \rho \) is the is the density of the fluid
\( v \) is the speed of the object relative to the fluid
\( A \) is the cross sectional area
\( C_{D} \) is the drag coefficient – a dimensionless number.
Data
Area, A/ \( cm^{2} \) | 289 | 249 | 190 | 169 | 130 | 88 |
Terminal Velocity, v/ \( cms^{-1} \) | 1.66 | 1.70 | 2.02 | 2.12 | 2.31 | 2.66 |
Version
http://weelookang.blogspot.sg/2016/08/sypt2016-workshop-materials.html
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- Details
- Written by leongster
- Parent Category: 03 Motion & Forces
- Category: 02 Dynamics
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