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Old 02-02-2013, 07:07 PM   #11 (permalink)
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Interesting,
I am finally starting to get a handle on what the numbers you quote mean, can be a bit slow at times.

With the Tuna, it was near enough to template, 2.5:1, on side profile, but on plan view is at ideal wing cross section, 4:1.

I was thinking how can we take something from this, which one of these is the governing measure, or are they the outer limits that natural selection has shown to achieve the most efficient movement through water (or any fluid).

With the wing section I assume this means in wing form, that it theoretically can continue this to infinity at 4:1 as the minimum drag form, where as with the body of rotation is at 2.5:1.

So with motor vehicles in ground effect (mirror) we have some elements of both of these characteristics, it is like a body of rotation, but has flatened sides, top, bottom etc, which give it some wing character.

Do we need to consider our vehicles in this manner and take some elements from each profile to best address the aerodynamic drag?

Don't know what or how, just playing with ideas.

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Old 02-05-2013, 06:50 PM   #12 (permalink)
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to consider

Quote:
Originally Posted by Tesla View Post
Interesting,
I am finally starting to get a handle on what the numbers you quote mean, can be a bit slow at times.

With the Tuna, it was near enough to template, 2.5:1, on side profile, but on plan view is at ideal wing cross section, 4:1.

I was thinking how can we take something from this, which one of these is the governing measure, or are they the outer limits that natural selection has shown to achieve the most efficient movement through water (or any fluid).

With the wing section I assume this means in wing form, that it theoretically can continue this to infinity at 4:1 as the minimum drag form, where as with the body of rotation is at 2.5:1.

So with motor vehicles in ground effect (mirror) we have some elements of both of these characteristics, it is like a body of rotation, but has flatened sides, top, bottom etc, which give it some wing character.

Do we need to consider our vehicles in this manner and take some elements from each profile to best address the aerodynamic drag?

Don't know what or how, just playing with ideas.
here are some elements which led me to the 'Template.'
*Paul Jaray,who was employed at the Zeppelin works is given credit for the longitudinally asymmetric airship body (blunt nose with tapering tail),although Pierre Juliene (sp?)had flown a model airship of this form inn 1850.
*This airship form is the streamline body of revolution.
*Paul Jaray was the first to use the term 'streamline.'
*Jaray took an airship body and sliced it in half,longways,to create a 'half-body',or 'pumpkin seed',which today,remains one of the lowest drag forms ever measured as a road vehicle.
*The pumpkin seed has twice the drag as the streamline body it is derived from.
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*The streamline body of lowest drag has a fineness ratio of L/D= 2.1
*This form is unsuitable as an airship,as it flies like a fumbled football,makes the whole crew airsick,is unsuitable as a photographic or weapons platform.So while it does have the lowest drag,you'll never see it in service.
*As a 'bluff body' road vehicle in ground effect,this forms aft-body is a bit too steep to protect the boundary layer and is prone to premature separation.
*Mair and Buchheim researched separation-free aft-body contours and reported that we should never exceed 22-23 degrees,respectively.
*The L/D= 2.5 streamline body is the shortest body which respects the 22-degree rule (it's conservative).
*It has a free-air Cd 0.04.
*As a half-body in ground proximity it has Cd 0.08.
*When narrow wheels and tires are added the drag goes to Cd 0.12.
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As a 'pure' half-body it would make for a 'wide' vehicle.The convention (if there actually is such a thing) is to narrow the body in plan,morph it into more of a rectangle in section for the passenger compartment,then re-morph it back into a more streamline body section for the tail.
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Some of the researchers or teams who have worked with the pumpkin seed are:
*Paul Jaray
*Walter E.Lay
*Elliott G.Reid
*Heald
*Fachsenfeld
*Kamm
*Reid Railton's 'Railton 'Mobil' Special'
*Jean Andreau's 'Thunderbolt'
*MG EX 181
*Mickey Thompson's 'Pumpkinseed'
*Walter Korff's dry lakes streamliner
*Doug Malewicki's' California Commuter'
*AeroVironment/GM Sunraycer
*Honda Dream I,II,III
*Cal Poly
*MIT
*University of N.Texas
*B'o'chum University,Germany
*other university solar race teams
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*It looks like the side elevation of the vehicle should stay close to the 'Template' and then for plan-view,since the vehicle is 'narrow',lean towards the 4:1 'Section' and do our best to blend it all together.
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I'm looking at some other teardrops and one has a little more aggressive early curvature like your NACA 0039
section and I think what you have would make a fine tool to work with,especially since you can get such specific vectors at any position.
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I'll never 'finish' looking at this stuff,but I think we're closing in on a useable 'Rosetta Stone' for decyphering the air.
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Old 02-05-2013, 08:29 PM   #13 (permalink)
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Quote:
Originally Posted by aerohead View Post
--------------------------------------------------------------------------
*It looks like the side elevation of the vehicle should stay close to the 'Template' and then for plan-view,since the vehicle is 'narrow',lean towards the 4:1 'Section' and do our best to blend it all together.
--------------------------------------------------------------------------
I'm looking at some other teardrops and one has a little more aggressive early curvature like your NACA 0039
section and I think what you have would make a fine tool to work with,especially since you can get such specific vectors at any position.
--------------------------------------------------------------------------
I'll never 'finish' looking at this stuff,but I think we're closing in on a useable 'Rosetta Stone' for decyphering the air.
Outside everything else you wrote which is full of aha! moments and I always get more insight,

That last part, 2.5:1 template over the top and 4:1 down the sides, pretty much throws us back into the range of the bluefin tuna and other aquatic kin.

Thee 0039 equation & spreadsheet has been great to be able to throw numbers in and study the outcomes and angles and that's why I was looking for an equation to work with, just think it's much easier to take a set of numbers out, mark them on the sectional areas, then cut and join up than trying to set angles as you go.
I do need to go back and revise the spreadsheet to allow the use of different curvature for the x & y coordinates, with the new knowledge that I have absorbed.

I think you are half right with the rosetta stone, but no doubt, once you have whaqt you think is the "perfect form", another stone will be turned over to reveal even more details of perfection.

Last edited by Tesla; 02-05-2013 at 08:36 PM..
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Old 02-06-2013, 07:15 PM   #14 (permalink)
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perfect

Quote:
Originally Posted by Tesla View Post
Outside everything else you wrote which is full of aha! moments and I always get more insight,

That last part, 2.5:1 template over the top and 4:1 down the sides, pretty much throws us back into the range of the bluefin tuna and other aquatic kin.

Thee 0039 equation & spreadsheet has been great to be able to throw numbers in and study the outcomes and angles and that's why I was looking for an equation to work with, just think it's much easier to take a set of numbers out, mark them on the sectional areas, then cut and join up than trying to set angles as you go.
I do need to go back and revise the spreadsheet to allow the use of different curvature for the x & y coordinates, with the new knowledge that I have absorbed.

I think you are half right with the rosetta stone, but no doubt, once you have whaqt you think is the "perfect form", another stone will be turned over to reveal even more details of perfection.
Yeah,it's a bit of a joke to presume that for so many types of vehicles manufactured that there would ever be a one-size-fits-all template.
What is a big help for us though,are a number of remarkably efficient vehicles of different types which have already been 'pulled off,' which we can consider when looking at a specific project.
FYI,if you haven't seen a copy of Wing Theory,by Abbott and von Doenhoff, it's full of location vectors for hundreds of wing sections.You could construct anything NACA ever looked at.Nearly.

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