Optimisation

By using FloEFD integrated in Catia V5 we were able to find the optimised shape of Hiko.

How wide should the wing root be?

The first calculation I made was the most simple with a single parameter: the width of the wing root

The optimum width seems to be 39mm

I tried from 30mm to 70mm. In the calculation volume i chose (which is not the complete plane) the drag force at 5 m/s varied from 430 mN to 370 mN


Another example: the V-tail

I tried to find a correct shae for the V-tail by changing the tension of tangents of the guiding curbes of the leading and trailing edges

I however didn't choose the optimum shape but the third best shape.

Indeed the optimum shape would have given a thin and fragile V-Tail with not enough area. But the one I chose only had 1% more drag with enough area to stabilize the plane and to be strong enough.

Between all the shapes that FloEFD tried, the "worst" shape had 9% more drag than the best one


glimps of the results

If you want to see how this FloEFD composant looks like, here is a glimps of the Multiparametric optimization window