Example 3.4.1.
Review ModelΒ 1.3.3. Consider how lift changes with respect to each of the parameters.
Consider \(\rho\) the density of air. If the other parameters remain constant (only density changes), then the model looks like
\begin{align*}
L & = \frac{1}{2}\rho s C_L v^2\\
& = \left( \frac{1}{2} s C_L v^2 \right)\rho\\
& = k \rho.
\end{align*}
All we used is commutativity of multiplication. We can see that lift (\(L\)) changes linearly with respect to air density (\(\rho\)).
Consider \(s\) the surface area of the airfoil (wing or propeller). If the other parameters remain constant (only surface area changes), then the model looks like
\begin{align*}
L & = \frac{1}{2}\rho s C_L v^2\\
& = \left( \frac{1}{2} \rho C_L v^2 \right)s \\
& = k s.
\end{align*}
We can see that lift (\(L\)) changes linearly with respect to surface area (\(s\)).
Consider \(C_L\) the coefficient of lift of the airfoil. If the other parameters remain constant, then the model looks like
\begin{align*}
L & = \frac{1}{2}\rho s C_L v^2\\
& = \left( \frac{1}{2} \rho s v^2 \right)C_L \\
& = k C_L.
\end{align*}
We can see that lift (\(L\)) changes linearly with respect to the coefficient of lift (\(C_L\)).
Consider \(v\) the velocity. If the other parameters remain constant, then the model looks like
\begin{align*}
L & = \frac{1}{2}\rho s C_L v^2\\
& = \left( \frac{1}{2} \rho s C_L \right)v^2 \\
& = k v^2.
\end{align*}
We can see that lift (\(L\)) changes quadratically with respect to velocity (\(v^2\)).
How can we apply this knowledge? Lift changes linearly with respect to all parameters except for velocity. If greater lift (to handle greater weight) is needed, velocity provides bigger bang for our buck than any other change.

