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Cd 0.38
Just to illustrate some of the variability of shapes with identical Cd
http://i1271.photobucket.com/albums/...titled1_24.jpg http://i1271.photobucket.com/albums/...d2/06-2826.jpg http://i1271.photobucket.com/albums/...titled19_3.jpg http://i1271.photobucket.com/albums/...titled1_19.jpg http://i1271.photobucket.com/albums/...titled9_19.jpg http://i1271.photobucket.com/albums/...titled8_19.jpg |
I just don't understand.
How can the Smart car have the same Cd, yet have such a massive wake ? The wake of the Z-28 is tiny in comparison. Are the vortices just more controlled in that design, or what ? |
Cd (a dimensionless number) is what's being asserted. But I'm wondering for an equal A (area) does the height/width ratio have any impact? The Template would be .5, my car closer to 1. The Smart could be over 1.
This is based on the sides having twice the taper of the top. |
how can
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*It has extremely good sectional density,displacing the air nicely with it's leading edges for complete flow attachment,and gradual reduction in cross-section allowing separation-free flow to the truncation,with perfect pressure recovery. *It's fineness ratio is adequate for Cd 0.38. *While it DOES have a relatively large wake,the base pressure is higher due to the careful contours and pressure recovery upstream.Just like a 2015 Ford Econoline which shares the same Cd. http://i1271.photobucket.com/albums/...titled9_15.jpg *It's 'Stromform' nose is of the lowest drag. http://i1271.photobucket.com/albums/...Untitled24.jpg *It's the only car with a proper K-form truncation. *It has zero-induced drag penalty. *There is essentially zero vorticity. *The base pressure of the Z-28's wake will be the same as at it's early separation point,way forward on the back slope.Very low pressure! Quite a penalty! |
height/width
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They varied the width of their airfoil-shaped model from around 230mm,to 1,000mm,holding the height constant,and recorded the same Cd, on a frontal area basis. Any car of any scale will have an identical Cd as long as Reynolds number is accounted for.They call is dynamic similarity,or verisimilitude. The tunnel velocity must be such that a turbulent boundary layer is guaranteed. |
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same reaction
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http://i1271.photobucket.com/albums/...titled10_1.jpg http://i1271.photobucket.com/albums/...titled16_4.jpg :D |
thanks Phil. This all gives me hope that my Kamm efforts are the way to go.
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Kamm efforts
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Darin's Honda proved that it's not a 100% solution though.I suspect that there was drag reduction,but the engine didn't react favorably to the mods. Chrysler and Dr. Gino Sovran warned about gear-matching requirements.Hope you don't hit a snag. |
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Back when I had the 1961 VW panel van, I thought about two Porsche duck tails, vertical on the sides, to create what I would verbalize today as a virtual plan taper.
More for directional stability than downforce, like a shuttlecock. |
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Once I'd hung around here for a while, I leaned more toward a rectangular 4" torus fed with the pumped engine cooling air, with louvers punched lengthways at the proper angle to form a Coanda nozzle on all four sides.
Today though, things are different. The news out of Manchester University: The future of flight: plasma aircraft wings | News & Events | Manchester Metropolitan University Quote:
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Page 2 Why are many UFOs an aerodynamic, saucer shape? Why are many UFOs an aerodynamic, saucer shape?, page 2 http://forums.pelicanparts.com/uploa...1446563860.jpg Quote:
How long before our cars start glowing blue? |
Puddle lights? we don' need no stinking puddle lights!
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I need plasma wings on my belly pan!
And spinner moon discs. ;) |
I'm out of state, and writing on my NOok tablet; so this is painful, but Plasma Actuators.
Popular Science, November 2015, page 26. =) Edit: searching to find this thread, I see this has been discussed before. In fact I was commenting on it in this thread last July. The memory is the first to go. Or is it the knees? Anyway, here's a Wikipedia entry on Plasma Actuators |
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