Dear Members,
this is my first post, glad to be part of this board. Know some of You have huge knowledge, this why I let myself to start topic in here. Been building my bike for almost 7 years, now its time to work on better aero, I was inspired by moto gp bikes.
I had to options do it just for look, are do all necessary calculations, I choose second way.
What I want to achive is better flow all over the bike, separat flow and reduce drag. I count also on better stability in to the corners (with "stock" look of the bike).
Waiting for feeback.
Lets start.
Im using aircraft science knowledge to make them work in my case, am I correct I don't know but if values will resonable I guess I will be. When we look at the bike from above it has approximately shape to tear drop, so I looks like wing in cross-section. So I think when we want to make vortex generators we can use same calculation as aviation.
air density - motorcycle (yes)
chord length - motorcycle length
dynamic Viscosity of air - set value
At the end we have stall speed, copy paste (Sumontro Sinha)
Stall speed is the speed where a wing loses lift and adds a lot of drag.
Should be lentgh from end of side fairing to the end of the bike.
I only think now about upper stream of air (fastest air) as its most important for us,
second side of bike is equal (I know exhaust).
The exact formula is
V = √( 2 W g / ρ S Clmax )
V = Stall Speed
W = Weight of the aircraft
g = 9.81 (Acc. Due to Gravity)
ρ = Density of Air
S = Wing Area
Clmax = Coefficient of Lift at Stall
Wing area is our whole bike (of course not in 100%) but I will count it as a length and from highest point to the ground.
Another value which I need to solve is Coefficient of Lift at Stall which is angle of attack,
I will take value from center line of the bike (from above) to maximum angle of bike turning point.
All these will let me to get Reynolds Number which I need to determine the height of my main wing and then.
Drawings and some pictures of my test.
Here is a test with strings, speed was about 70km/h.
What I think I see is no chaotic flow. No good result. Tail section is completely wasted.
Do not understand why flow is going down (this could increase wheele symptom).
What I want to achive.
During the weekend I did some calculations ang get some numbers. I cut cardboard form of main wing (to be honest there should be 3 of them across whole hight of the bike).
All numbers are for rectangular vortex generator beacuse I have good explenation how to do this. Anyhow rectangular profile is good as it self because of a big operating surface.
After I get size of the wing I calculate winglet for it basing on diameters of the wing.
Was thinking about profile, what I get its about 8mm maximum thickness, which should be 1/3 length from front of the wing. Need to read about it more. Shape should depand on Re number size.
After all I calculate best postions and hight for wing to be placed.
Back in a days I did also handle fairings, but know I think they should be a bit bigger (I change clip on's position to wider.
Pic. material:
What do You think about it?