You test separation and also just make sure it matches what it did when you put it on the wind tunnel model.henra wrote:andmarcush. wrote:But you correlate a modified experiment ,don´t you?That's exactly what I was wondering also (referring to both - the pitot arrays and the flow viz).good luck ,I don´t buy it.It´s useless crap to me ,as is the flowwiz voodoo (where is the sense of applying a liquid to a surface and then go around a circuit at x speeds ,x-acceölerations and completly unpredictable influences ? I never saw any team actually video capturing their flowviz runs on track which would make it all a lot more worthwhile doing
That massive grid will have significant effects upstream and will yet only measure individual (read fluctuating) data in a turbulent flow. So two effects that make me both wonder what you can really read from the results.
And for the flow- viz: For what speed do you want to determine the actual flow? I'm pretty sure that the local speed and direction in an area passed by a rotating vortex will change so much that at the end of one lap you only have a big mixture of traces. It might work if you want to identify if flow separation occurs under any circumstance at a given location but beyond that? I don't see how you could correlate certain elements of a flowviz trace with a certain speed or behaviour of the car in a certain condition !?
Teams rely on the fact that the flow vis do not have a strong dependance on speed - they do depend on car's attitude (yaw especially. Any way you can always correlate the pictures with the vehicle dynamics data of the run and check for ranges (e.g. you see that you had yaw form -5° to 5° during the lap, you expect to see the swept pattern of the vortex being in between where you predicted it to be at -5 and at +5)henra wrote:And for the flow- viz: For what speed do you want to determine the actual flow? I'm pretty sure that the local speed and direction in an area passed by a rotating vortex will change so much that at the end of one lap you only have a big mixture of traces. It might work if you want to identify if flow separation occurs under any circumstance at a given location but beyond that? I don't see how you could correlate certain elements of a flowviz trace with a certain speed or behaviour of the car in a certain condition !?
Nice catch, lots of ressources and finetuning going into that area.Matt Somers wrote:Tyre Squirt Slot added to the RB9 (Not sure if it's on both cars yet)
https://pbs.twimg.com/media/BJ_gf6wCUAAYWMk.jpg:large
I would expect some speed dependency in areas where vortices are present. The existance, angle, diameter and postion of these vortices will ususally change with the speed. And that is where I would exect severe difficulties in correlating traces with the situation at a certain speed or track positionshelly wrote: Teams rely on the fact that the flow vis do not have a strong dependance on speed - they do depend on car's attitude (yaw especially. Any way you can always correlate the pictures with the vehicle dynamics data of the run and check for ranges (e.g. you see that you had yaw form -5° to 5° during the lap, you expect to see the swept pattern of the vortex being in between where you predicted it to be at -5 and at +5)
and:I agree about detecting speartaion with owen: you never want ot see detached patterns on the car at condition (drs or drd excluded) so you use paint to check that - for example the loss of boundary layer energy and late separation along the sidepod is crucial from 2012 because of coanda exhaust.
OK, Agreed, that makes sense.Owen.C93 wrote: You test separation and also just make sure it matches what it did when you put it on the wind tunnel model.
Did they get rid of the resonating chamber on exhaust?
It's between the engine and exhaust.Mr.G wrote:Did they get rid of the resonating chamber on exhaust?
yes indeed...seven elements is a lot. But Red Bull's engineers (and Ferrari's) can't go much further: increasing the number of overlapping wings means to reduce the gaps in between them, which leads to a greater boundary layer prominence over "clean" air...very bad if you want to keep the airflow to stay adherent to the wing. It also causes a slight loss of high pressure on top of the wing.zac510 wrote:RBR must have hired some Gillette engineers (just keep adding more blades!)