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Tracking / Autocross / HPDE / Drifting What these cars were built for! |
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01-01-2014, 04:35 AM | #15 |
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I'd love an active wing for the track!
How would it engage? I'm thinking it would be best to be full on all the time, unless throttle was down past half way, or something of that nature. |
01-01-2014, 10:33 AM | #16 | |
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For every instance where you put your foot down early, lift past your engagement point, or tap your brakes, you've introduced a new variable to compensate for. Ask me how I know. -Arduino controlled wings are a bad idea on a racetrack! |
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01-01-2014, 11:39 AM | #17 | |
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What are you using for CFD analysis? Is the wing dedicated specifically toward this car? It seems you're using a pre-existing blade design. Why not tailor it specific to the FRS/BRZ body? |
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01-01-2014, 12:12 PM | #18 | |
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2013 SWP BRZ Build Thread: http://www.ft86club.com/forums/showthread.php?t=38781 |
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01-01-2014, 01:09 PM | #19 |
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I'm more concerned with the fence plate shapes you have on the diffuser design...which has bothered me ever time I've seen those images. Why unnecessarily slow the air down and increase pressure (which is the opposite of what a diffuser is designed to do)?
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01-01-2014, 02:04 PM | #20 |
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The diffuser doesn't look like that anymore. The first picture on the second set has the verticals flat now, but that is a different project.
Unless someone else knows of a loophole or a hidden rule, I don't think this wing will fit into any SCCA classes because of the mounting location. So I'm just going to build it for fun. |
01-01-2014, 02:14 PM | #21 |
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phastafrican; The control system is going to be an option I've built with my own custom custom non-arduino system that uses latter logic. It will have brake pedal, gas pedal, and G-senor inputs, and much more user friendly than arduino. Again it will be an option to the fixed position wing.
CSG Mike; The CD/CL is .0136 at optimal angle. This is very low. The aerfoil design is very similar to most "GT" style wings. I think most of the wings on the market are pretty crap and overpriced. They are more for show than function. |
01-01-2014, 02:38 PM | #22 |
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It's very easy to get a high drag/downforce ratio in free-flowing air over just a blade.
What have you modeled this in to get your data? Without data, it's just another generic wing. Since you haven't picked up on it, this is why I'm questioning you: your mounting solution introduces more drag than the wing will ever make, even at maximum AoA at the verge of stalling. I don't need to do any CFD to know that, simply due to the design. |
The Following User Says Thank You to CSG Mike For This Useful Post: | plucas (01-01-2014) |
01-01-2014, 02:53 PM | #23 | |
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01-01-2014, 03:06 PM | #24 |
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CSG Mike; The data is from table sets for the wing profile. It is a well documented profile and I did the calculations for a reynolds number of 100,000 and Ncrit=9, for sea level air. This gives a maximum Cl/Cd of 156.5 @ 6.25 degrees. This does not take into account the mounting solution and I understand it will have a constant drag coefficient that I have yet to calculate.
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01-01-2014, 03:16 PM | #25 |
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Sounds like you're committed to testing this out. Looking forward to the results. It's not a novel idea, but your approach appears innovative.
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01-01-2014, 03:16 PM | #26 | |
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01-01-2014, 03:35 PM | #27 |
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It does take into account induced drag. The optimum angle for down-force is around 13 degrees and the induced drag almost doubles the drag because of it. CL @ 12.5 degrees = 2.0391.
These numbers are optimal and with perfect, laminar airflow. The conditions will be much less optimal on the car, but It's good to start with a nice optimal design to get a better real world one. Last edited by Rosticles; 01-01-2014 at 04:38 PM. Reason: forgot to post cl |
01-01-2014, 05:12 PM | #28 |
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This sounds like you are getting a head of yourself. Are you pulling these Cl and Cd numbers from a table? Also you state that these numbers are optimal with perfect laminar airflow. You know that most cars start to transition to turbulent flow at around 60mph. The airflow will not be laminar on this wing at 100mph. I bet that wing stalls at 13 degrees.
A wing will work very different on the back of a car than in free stream air. I have done extensive work with this using cfd. If you want some help with this, let me know. My background is an engineer specializing in fluid flow and heat transfer. |
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