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Strut fairing questions.
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andynfultz(at)bellsouth.n
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PostPosted: Sun Sep 16, 2007 4:18 pm    Post subject: Strut fairing questions. Reply with quote

John,

Would you mind sharing what that "aerodynamic rule of thumb" is? I'm
about to start working on my 7/8" struts in the next few weeks and would
like to streamline them as well. I do know that a round tube causes a lot
of drag. Thanks.

Andy F.

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dave



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PostPosted: Sun Sep 16, 2007 4:35 pm    Post subject: Re: Strut fairing questions. Reply with quote

I have to check from Hoerners book but i think it around 4 to 1 ratio

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propellerdesign(at)tele2.
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PostPosted: Mon Sep 17, 2007 12:20 am    Post subject: Strut fairing questions. Reply with quote

Hi

It depends on the Reynolds number, a cyl (tube) with Re <10^5 have drag coefficient 1 - 1,3, and with Re >10^6 = CD 0,30

With an airfoil of length 3:1 (0,333) and Re >10^6 = CD 0,04
with a Re under 10^5 the length have to be 5:1 (0,20) to get same drag CD 0,04

a 2" diameter tube at 100 MPH have Re 1,56*10^5
8" long and Re is 6,26*10^5 and CD will be 0,012 with reference to the surface area

so with say total 10 meter of 2" tube the drag will be 60-80 kg
and with airfoil 3 kg at 100 MPH

And a NACA 67-020 or NACA 67-025 will have little more then half the drag a NACA 0020 - 0025 will have if made correct.

Jan
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Float Flyr



Joined: 19 Jul 2006
Posts: 2704
Location: Campbellton, Newfoundland

PostPosted: Mon Sep 17, 2007 4:43 am    Post subject: Strut fairing questions. Reply with quote

Dave check the ratio on the extruded spars on your floats and let us know.

[img]cid:201543212(at)17092007-235D[/img]
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PostPosted: Mon Sep 17, 2007 11:34 am    Post subject: Strut fairing questions. Reply with quote

All,

For any of you having a little trouble interpreting Jan's formulas, here's the laymens formula for determining fairing sizes as I remember it;

For every inch of thickness of the part you want to streamline, you need a fairing 4.25 times wider. In other words, if you have a one inch round strut tube, you will need a streamline fairing with a 4.25 inch wide chord. Interestingly, the shape of streamlined chromoly and aluminum for aircraft generally do not meet this rule, as for the most part they have too narrow of a chord (Go figure?)

Now this is just a general rule of thumb, and it's off the top of my head. So if you want more technical than that, talk to Jan...

Paul Seehafer
Kitfox IV 912ul amphib
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propellerdesign(at)tele2.
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PostPosted: Mon Sep 17, 2007 12:31 pm    Post subject: Strut fairing questions. Reply with quote

Well spoken.

Re number is the length in mm (millimeter) times airspeed in m/s times 70. (there is a formula for inch, feet and miles too)

in short, wing struts is UNDER CRITICAL Re. so need 4 to 1 or 5 to1 in length versus thickness. and / or laminar layer control ( Think golf ball) to trip the boundary layer into TURBULENT layer that have energy to follow the airfoil.
can be made of Dyno tape (old one) with big V typed all the way. or cut length vise with a zigzag scissor (for fabric) and the cut turned into the airstream, applied both side of wingstrut. at highest point, or just forward of.

CD is Drag Coefficient that relates to something like wet area or frontal area (different coefficients)
To get the actual drag, CD times the reference area times Dynamic pressure. simple as that.

and at level flight drag equal thrust, and lift equal weight (almost)

Jan
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