I'm working on a school project about the aerodynamics of an helicopter blade. I'm trying to adapt my aerodynamics class ( centered around planes wings mostly ) to this case.
In our class, we used what we called the integrals of Glauert and more specifically, this integral : $$ \int_{0}^{\pi}\frac{\cos\left(nx\right)} {\cos\left(\theta\right) - \cos\left(x\right)}\,{\rm d}x = -\pi\,\frac{\sin\left(n\theta\right)}{\sin\left(\theta\right)} $$ In the helicopter case, I need to evaluate a similar integral but with $\sin\left(nx\right)$ instead of $\cos\left(nx\right)$.
I found a beautiful proof of the first result in the book Inside Interesting Integrals by Paul Nahin ( page $60$ ) which uses recursivity. I tried to adapt it to the other integral using the formula $$\sin\left(\left(n + 1\right)x\right) + \sin\left(\left(n - 1\right)x\right) = 2\sin\left(nx\right)\cos\left(x\right)$$ $$ \mbox{Calling}\quad I_{n} = \int_0^\pi\frac{\sin\left(nx\right)}{\cos\left(\theta\right) - \cos\left(x\right)}\,{\rm d}x, $$ I find that $$ I_{n+1} - 2\cos\left(\theta\right)I_{n} + I_{n - 1} = \int_{0}^{\pi}2\sin\left(nx\right)\,{\rm d}x $$ but I then have a problem to solve the recursive equation be the result is $0$ or $\frac{4}{n}$ depending on the parity of n. I decoupled the system to get two recursive equations for the different parities :
- For $a_n=I_{2n}$, I get $a_{n+1}-2\cos(2\theta)a_n+a_{n-1}=8\cos\theta(\frac{1}{2n+1}+\frac{1}{2n-1}$)
- And for $b_n=I_{2n+1}$, I get $b_n-2\cos(2\theta)b_{n-1}+b_{n-2}=\frac{8}{2n-1}\cos(\theta)$
I entered these formula on Wolfram Alpha and got some really ugly results. I was thus wondering if a more simple formula could exist for my integral.
I also quickly looked at the wikipedia proof which uses residual theorems but I got lost quite fast...
Do you know some other way to evaluate this integral or maybe if it's possible to solve the recursive equations to get to a simpler result than the one from Wolfram ?
Thank you very much !