Big Bird pics
#61
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Hi Dave,
Great info, even thou Tom's minimal and smaller braces are not aero correct I had a feeling the smaller struts in the fashion he mounted them would be a lot less drag that some of the "X" bracing I have seen.
I haven't personally ran one that so high that I needed such thick supports and braces and your input is great info for future "higher" applications.
IF you don't mind, while you are crunching numbers give me your thoughts on these 2 different airfoil profiles. Sorry for the crappy photos, but I think you can get enough from them for your calcs. FYI, the lower one is the same as DL's so you probably already have the data.
Great info, even thou Tom's minimal and smaller braces are not aero correct I had a feeling the smaller struts in the fashion he mounted them would be a lot less drag that some of the "X" bracing I have seen.
I haven't personally ran one that so high that I needed such thick supports and braces and your input is great info for future "higher" applications.
IF you don't mind, while you are crunching numbers give me your thoughts on these 2 different airfoil profiles. Sorry for the crappy photos, but I think you can get enough from them for your calcs. FYI, the lower one is the same as DL's so you probably already have the data.
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Last edited by DR; 02-25-2005 at 09:57 PM.
#62
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Interesting stuff.
why the 50% greater cross section? was that due to the strength of round pole vs air foil shape? Still, the net result was 20% of the drag for an air foil shape even 50% larger is the main point here.
if you look at formula cars now, all struts are like the ones found on modern air planes. everything is covered, air foiled, naca ducted, etc.
Mk
why the 50% greater cross section? was that due to the strength of round pole vs air foil shape? Still, the net result was 20% of the drag for an air foil shape even 50% larger is the main point here.
if you look at formula cars now, all struts are like the ones found on modern air planes. everything is covered, air foiled, naca ducted, etc.
Mk
Originally Posted by worf928
A long long time ago in a galaxy far far away I did the drag vs. mass vs. strength analysis of round-profile suspension components on an open-wheel car vs suspension components of equal load capacity with a basic low-drag profile. The aero-shaped member needed to have about 50% more cross-section but the drag was something like 20% of the round one. The difference is greater for a longer component due to edge effects being more dominant on the shorty components.
In that same universe we did the analysis of round profile support wires on long wings. The drag penalty was a jaw-dropper. But, in that case the mass and cost penalty of doing something different was too great.
Don't ask me to repeat those analyses; I killed those neurons a decade ago with beer...
In that same universe we did the analysis of round profile support wires on long wings. The drag penalty was a jaw-dropper. But, in that case the mass and cost penalty of doing something different was too great.
Don't ask me to repeat those analyses; I killed those neurons a decade ago with beer...
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Originally Posted by DR
Great info, even thou Tom's minimal and smaller braces are not aero correct I had a feeling the smaller struts in the fashion he mounted them would be a lot less drag that some of the "X" bracing I have seen.
IF you don't mind... Sorry for the crappy photos, but I think you can get enough from them for your calcs. FYI, the lower one is the same as DL's so you probably already have the data.
If you cannot I'll give it a shot but I may need to add so many caveats that a cursory analysis is not usable.
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Hi Dave,
>I don't mind a bit.
Somehow I knew that :-)
>And yes, I do still have the profile from DL's wing. My concern with the aggressively cambered wing >is that the picture is not a true profile. Once you get 'exotic' on the camber small changes (or errors >due to perspective) can have disproportionate effects. Do you think you could get a true cross->section picture?
>If you cannot I'll give it a shot but I may need to add so many caveats that a cursory analysis is not >usable.
That is the best I have at the moment, it will be a week or so before I can take a photo of the profile myself.
I know what the manufacturer claims about this profile, but I am really curious as to your un-biased opinion.
Thanks in advance,
>I don't mind a bit.
Somehow I knew that :-)
>And yes, I do still have the profile from DL's wing. My concern with the aggressively cambered wing >is that the picture is not a true profile. Once you get 'exotic' on the camber small changes (or errors >due to perspective) can have disproportionate effects. Do you think you could get a true cross->section picture?
>If you cannot I'll give it a shot but I may need to add so many caveats that a cursory analysis is not >usable.
That is the best I have at the moment, it will be a week or so before I can take a photo of the profile myself.
I know what the manufacturer claims about this profile, but I am really curious as to your un-biased opinion.
Thanks in advance,
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Originally Posted by mark kibort
why the 50% greater cross section? was that due to the strength of round pole vs air foil shape?
![Smilie](https://rennlist.com/forums/images/smilies/smile.gif)
Now, if we were in F1 lala land we could have a component fabricated with non-uniform wall thickness over the cross-section, keep the mass down and keep the cross-section small.
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Originally Posted by DR
That is the best I have at the moment, it will be a week or so before I can take a photo of the profile myself.
I know what the manufacturer claims about this profile, but I am really curious as to your un-biased opinion.
When you get something from a flat angle send it to me and I'll see what I can see.
Better yet is to have Pierre take it over to his buddy and see what he thinks.
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Ahem,
Maybe the support for the wing could be nearer the roof where the hatch bolts to the body.. The extenders to support the wing would be on a slightly different plane, and would require a bit different support.. However, It could be sililar to the Rally Escort Cosworth cars that were in Group B racing..
It may allow the control of the variables while offering a better support point for the wing..
Oh, the supports could also be made from Carbon Fiber/Kevlar for strength and weight issues.. They could be laminated pieces molded to that compound shape, then glued and gel coated...
About cost, no comment there....
Good Luck Guys,
I'll just watch from the sidelines thank you..!
Maybe the support for the wing could be nearer the roof where the hatch bolts to the body.. The extenders to support the wing would be on a slightly different plane, and would require a bit different support.. However, It could be sililar to the Rally Escort Cosworth cars that were in Group B racing..
It may allow the control of the variables while offering a better support point for the wing..
Oh, the supports could also be made from Carbon Fiber/Kevlar for strength and weight issues.. They could be laminated pieces molded to that compound shape, then glued and gel coated...
About cost, no comment there....
Good Luck Guys,
I'll just watch from the sidelines thank you..!
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I don't claim to "know", and perhaps the splitter and wing I have just make my car slower, so more comfortable in the corners, but at least I have both. The wing is adjustable, the splitter is not. Of course a running motor would make it much quicker ![Frown](https://rennlist.com/forums/images/smilies/frown.gif)
Accusump did have metal shavings in it, so it was not working properly prior to the last motor's failure.....
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Accusump did have metal shavings in it, so it was not working properly prior to the last motor's failure.....
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Hi Stan,
>Of course a running motor would make it much quicker
So it is safe bet that your BFW will not send you into the air like a bird any time soon, right?
>Accusump did have metal shavings in it, so it was not working properly prior to the last motor's failure.....
Interesting, did the metal shavings come from the old engine, or from the accusump itself? I know what accusump will say, but I am curious as to your opinion.
>Of course a running motor would make it much quicker
So it is safe bet that your BFW will not send you into the air like a bird any time soon, right?
>Accusump did have metal shavings in it, so it was not working properly prior to the last motor's failure.....
Interesting, did the metal shavings come from the old engine, or from the accusump itself? I know what accusump will say, but I am curious as to your opinion.
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My (perhaps limited) understanding of the accusump would make me wonder how the accusump itself would generate shavings. Doesn't seem too likely it would fail, the piston movement would be relatively slow with only low pressure, right?
What concerns me is that the first motor failed due to a #8 rod bearing failure, and I really don't know why. If the accusump was in-operative before that point, wouldn't the #2/#6 bearings have been likely to fail? I did find wear on other rod bearings as well though. The motor only had 15 track days on it, about 90 minutes per day.
Perhaps I ran the last motor too long on non-synthetic for break in, resulting in it's eventual failure. Then I didn't identify the problem with the accusump which resulted in the second motor failure.
I haven't decided whether I will replace all my oil lines this time, as well as my System 1 filter.....
What concerns me is that the first motor failed due to a #8 rod bearing failure, and I really don't know why. If the accusump was in-operative before that point, wouldn't the #2/#6 bearings have been likely to fail? I did find wear on other rod bearings as well though. The motor only had 15 track days on it, about 90 minutes per day.
Perhaps I ran the last motor too long on non-synthetic for break in, resulting in it's eventual failure. Then I didn't identify the problem with the accusump which resulted in the second motor failure.
I haven't decided whether I will replace all my oil lines this time, as well as my System 1 filter.....
#74
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Something like this?
Borrowed from the internet.
Supports running back from the hatch hinge area to join
with vertical to hold mongo rear wing in place.
![](http://forums.rennlist.com/upload/rally_car_wing.jpg)
Borrowed from the internet.
Supports running back from the hatch hinge area to join
with vertical to hold mongo rear wing in place.
![](http://forums.rennlist.com/upload/rally_car_wing.jpg)
Originally Posted by blau928
Ahem,
Maybe the support for the wing could be nearer the roof where the hatch bolts to the body.. The extenders to support the wing would be on a slightly different plane, and would require a bit different support.. However, It could be sililar to the Rally Escort Cosworth cars that were in Group B racing..
<snip>
Maybe the support for the wing could be nearer the roof where the hatch bolts to the body.. The extenders to support the wing would be on a slightly different plane, and would require a bit different support.. However, It could be sililar to the Rally Escort Cosworth cars that were in Group B racing..
<snip>
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Originally Posted by Pierre Martins
To cut a long story short - I've bought a wing with a gurney flap on top. My car is not strong enough to handle a lot of drag so i'm gonna set the main wing for turbulance only, and use the adjustable gurney flap for downforce when i need it. Here's the clincher - the flap will be spring-loaded and cable operated from inside the car so i can adjust it when and where i want.
Let you minds flow on that one for a while... You can even have a servo motor to electronically adjust downforce in the corners you want, and minimum downforce down the straights.
Let you minds flow on that one for a while... You can even have a servo motor to electronically adjust downforce in the corners you want, and minimum downforce down the straights.
Most racing groups ban "moveable aerodynamic devices" but open track days and DE's don't care. It's pretty cool to see it in action, like wathcing Jim Hall's old Chaparrals.
![](http://www.jeepvideos.com/mpeg/pics/wurth_jan_03_jzr_wing.jpg)
![](http://www.jeepvideos.com/mpeg/pics/wurth_jan_03_jzr_wing_track.jpg)