Blue,
Could you clarify this for me ? "...short and fat is better than long and skinny..." that would be with the same frontal area, right ?
thanks
roy
Nope, that's one of the big misconceptions. Taking the same volume from a long and skinny streamliner and rearranging it in a short and fat profile creates
more frontal area, less wetted area, more laminar flow and as little as
one-forth the drag (presuming neither car had any separation).
Willie,
As airfoil sections for wheel driven LSR, we need to look at NACA 66-018 and 021 sections. If we have a body of revolution, we can go even fatter. A "body of revolution" is when we create a body from a profile like turning it on a lathe. A body of revolution can be much fatter than a wing profile for the same peak velocity and pressure recovery.
One of the more important things we can learn from these profiles is the reflex in the pressure recovery. This is where we close the back of the vehicle very abruptly and then reduce the closure angle. This reduces length, wetted area, and is much lower in drag than a straight taper. Not to criticize LSR too much, but the idea of this straight, "7 degree" closure has got go away. It died in aerodynamic science over 70 years ago. On my last drag reduction project, I closed the fuselage at a peak of 18 degrees to PREVENT separation. Along the wing trailing edge vortex sheet (the actual streamline), the angle peaked at almost 30 degrees. Tufting showed no separation where the more gentle profile had previously separated. I do not recommend these angles, each application requires analysis.
With no turbos, a lot of detail work by Mountain Air Aviation and the owner, and the described drag reduction, the aircraft is now 55 mph faster than stock: 343 vs. 287 mph on the Reno Sport course.