by blaktopr » Wed Nov 05, 2008 12:17 am
Here is my take from testing and my mouse is crap! As you read this, look at the black areas as fuel puddleing and not being burned thoroughly leaving the sooty black residue. The cleaner spots, had higher speeds keeping some fuel more suspended, until a radical speed increase, dropping the fuel out. I tried to illustrate the pic. Blue lines airflow. Red lines, faster airflow. Magenta, even faster around plug. Yellow is fuel. The three yellow lines on lower right hand corner leading to the quench pad would be under turbulent conditions with larger droplet size congregateing on the wall below it. I am only speculating this without testing your head, but referencing to mine, so don't kill me. The black spot between the two valves and below the plug is where the fuel vortex is and is loose fuel. Burned slower with less O2, so black. Clean ring across plug where speed of air and fuel matched out of seat area, more burned uniformly. Dark area over that clean ring, speeds fast out of seat driving some fuel to ram in and pile up a little then being pushed around toward the exhaust but unable to be drawn back into the fast airstream so just stays there as a thinish layer. Same goes for under the intake toward the exhaust. ( I am referencing top/bottom to the pic only.) The two paths meet on the cylinder wall. Some of the blacking on the exhaust valve, fuel just slowly trapped and moving around in a circular pattern and side to side. Black at the edge of the exhaust valve same side of intake, (no yellow, sorry) fuel separating as speeds increase across the margin. Yellow dots around intake valve, fuel droplets stuck to the edge of the seat cut and margin. Dark area around intake at chamber wall over cylinder wall, same high airspeed, fuel separation as other spots of chamber. Most chambers are smooth, yet to combat some separation problems in the runner, we make it very course. The chamber is treating the fuel as if you polished the intake runner.
As for the spot on the valve inside the runner, over the severe dogleg, That I think is there because at the higher airspeeds not only does air not want to make that sharp turn, but also the fuel. So both tends to follow the straightest path to the valve and not even touching that section of the valve. If any fuel separates to behind that buldge and forms on the walls, the airspeed is too slow back there and the high pressure area pushes it down along the wall utilizing only the seat and not the face of the valve, therefore not touching that part to leave any fuel and depositing it in that area in the chamber on the wall side.(I think I have the port bias right) Leaving the black deposit. Just trying to contribute.
Chris
Chris Sikorski