{source}
<?phprequire_once JPATH_SITE.'/TTcustom/TT_contentparser.php';
//include 'TT_contentparser.php';
\(parameters = array( "topicname" => "02_newtonianmechanics_3dynamics", //e.g. 02_newtonianmechanics_2kinematics
"modelname" => "sypt2017wprkshop88"); //e.g. airpuckconstantvelocity.trz
echo generateSimHTML(\)parameters, "TRZ");
?>
{/source}
Theory
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
end faq