Re: Aerodynamic modifications
Found some time to look. Confused Dago with Red Barron, maybe because they're both, 'red'. Dago looks like they sported the same tips throughout.
Dago/ original PM tips are pretty bad.
Dago could have been faster. The sharp corner buys separation with the laminar airfoil section, and would also cause separation for a conventional section. They should have blended the vertical end plate in with a generous surface curvature like is seen on blended winglets. The 45 degree scarf is still a good idea, but having the end follow the upper surface curvature on the aft end of the airfoil, like Red Barron, is not. Original winglets had the same sharp corner that compromised their performance.
Wing tip vortices cause induced drag by some definitions, but they also cause flow disturbances and 3D boundary layer build-up on the wing upper surface as seen in the picture.
A couple of ways around that is to thin the tip and delete the aft surface as seen on stock Cubs, or minimize the wing tip chord as is found on soaring birds. Soaring birds also get the wingtip vortex out of the plane of the wing. Birds that fly through bushes and trees have low aspect ratio wings and the tip chord is long to get the wing loading down for maneuver in tight spaces.
The Formula guys have figured it out with tips that come to a point at the trailing edge. That fast biplane does the same essentially, and they even applied the idea to the prop tips.
Boeing's new airplane models minimize tip chord and the vortex is out of the wing plane due to wing deflection at 1g. They also sweep the tip because the shock wave wants to unsweep at the tip.
Anybody know how we got from Red Barron type tips to Voodoo/Strega tips?
Originally posted by Wild Bill Kelso
View Post
Dago/ original PM tips are pretty bad.
Dago could have been faster. The sharp corner buys separation with the laminar airfoil section, and would also cause separation for a conventional section. They should have blended the vertical end plate in with a generous surface curvature like is seen on blended winglets. The 45 degree scarf is still a good idea, but having the end follow the upper surface curvature on the aft end of the airfoil, like Red Barron, is not. Original winglets had the same sharp corner that compromised their performance.
Wing tip vortices cause induced drag by some definitions, but they also cause flow disturbances and 3D boundary layer build-up on the wing upper surface as seen in the picture.
A couple of ways around that is to thin the tip and delete the aft surface as seen on stock Cubs, or minimize the wing tip chord as is found on soaring birds. Soaring birds also get the wingtip vortex out of the plane of the wing. Birds that fly through bushes and trees have low aspect ratio wings and the tip chord is long to get the wing loading down for maneuver in tight spaces.
The Formula guys have figured it out with tips that come to a point at the trailing edge. That fast biplane does the same essentially, and they even applied the idea to the prop tips.
Boeing's new airplane models minimize tip chord and the vortex is out of the wing plane due to wing deflection at 1g. They also sweep the tip because the shock wave wants to unsweep at the tip.
Anybody know how we got from Red Barron type tips to Voodoo/Strega tips?
Comment