I’m suspicious of anyone who knows the second verse. 

-----Original Message-----
From: "JR" <[EMAIL PROTECTED]>
To: "Tom Wilksch" <[EMAIL PROTECTED]>, "Discussion of issues relating to 
Soaring in Australia." <[email protected]>
Date: Tue, 20 Jun 2006 22:51:20 +0930
Subject: Re: [Aus-soaring] Bent up wing outer panels

Well he only lasted 2 minutes with me, if they cant sing the first line of
advance australia fair I hang up
----- Original Message ----- 
From: "Tom Wilksch" <[EMAIL PROTECTED]>
To: "Discussion of issues relating to Soaring in Australia."
<[email protected]>
Sent: Tuesday, June 20, 2006 10:30 PM
Subject: Re: [Aus-soaring] Bent up wing outer panels


> yes, they seem to take 10 minutes to get to the point
>
> ----- Original Message ----- 
> From: "Patching" <[EMAIL PROTECTED]>
> To: "Discussion of issues relating to Soaring in Australia."
> <[email protected]>
> Sent: Tuesday, June 20, 2006 9:05 PM
> Subject: Re: [Aus-soaring] Bent up wing outer panels
>
>
> Oh yes inddeedy, they have a very interesting way of communicating. Fast?
> I'm not too sure of that.
> Ian P
> ----- Original Message ----- 
> From: "JR" <[EMAIL PROTECTED]>
> To: "Discussion of issues relating to Soaring in Australia."
> <[email protected]>
> Sent: Tuesday, June 20, 2006 6:15 PM
> Subject: Re: [Aus-soaring] Bent up wing outer panels
>
>
> > Ian,
> > I spoke to the worlds fastest Indian on the phone last night, he was
> > trying
> > to convert me to another phone company
> > regards JR
> > ----- Original Message ----- 
> > From: "Patching" <[EMAIL PROTECTED]>
> > To: "Discussion of issues relating to Soaring in Australia."
> > <[email protected]>
> > Sent: Tuesday, June 20, 2006 1:10 PM
> > Subject: Re: [Aus-soaring] Bent up wing outer panels
> >
> >
> >> Hey caleb,
> >>  the kookas' all have a decided wing kink as well. Just goes to proove
> >> the
> >> everything stays the same, it just gets refined a little.
> >> See ya, I'm off to see the Worlds Fastest Indian.
> >> IP
> >> KPST
> >> ----- Original Message ----- 
> >> From: "Caleb White" <[EMAIL PROTECTED]>
> >> To: <[email protected]>
> >> Sent: Tuesday, June 20, 2006 1:01 PM
> >> Subject: Re: [Aus-soaring] Bent up wing outer panels
> >>
> >>
> >> > Hi Folks,
> >> >
> >> > I think this discussion needs some clarification as to what is
referred
> > to
> >> > as a ‘kink’. Are we referring the stepped taper (when viewed in plan
> > form
> >> > from above) as the ‘kinks’? In which case we are discussing the
desire
> > to
> >> > achieve an elliptical plan form (with the intent of achieving an
> >> > elliptical lift distribution) OR Are we discussing the stepped
changes
> > in
> >> > dihedral in which case we are talking about achieving elliptical
> > dihedral?
> >> >
> >> > As with all aircraft design the design of sailplane wings is a
> > compromise.
> >> > What is desirable is balanced with what is affordable to manufacture.
A
> >> > stepped planform and dihedral is an excellent example of ‘optimised
> >> > compromise’.
> >> >
> >> > Cheers,
> >> >
> >> > Caleb
> >> >
> >> > Kookaburra Precision Soaring Team
> >> >
> >> >
> >> > -----Original Message-----
> >> > From: Mike Borgelt <[EMAIL PROTECTED]>
> >> > To: "Discussion of issues relating to Soaring in Australia."
> >> > <[email protected]>
> >> > Date: Tue, 20 Jun 2006 12:46:06 +1000
> >> > Subject: Re: [Aus-soaring] Bent up wing outer panels
> >> >
> >> > At 11:57 AM 20/06/2006, you wrote:
> >> >>Dear All (Bernard E would read this as 'space' but I'll stay with the
> >> >>English)
> >> >>
> >> >>There is the limitation in two dimensional aerodynamics of a minimum
> >> >>in the induced drag coefficient of:
> >> >>
> >> >>     Cd (induced) = Cl squared divided by (Pi X Aspect
> >> >> ratio).  (Apologies, I haven't the time to write it out clearer.)
> >> >>
> >> >>So with an ideal lift distribution along the two dimensional wing
> >> >>planform, that is the lowest you can get the induced drag
> >> >>coefficient down to.  Induced drag relates to drag due to wing tip
> >> >>vortices (actually more complicated than just tip vortices but let
> >> >>us leave that for now).
> >> >>
> >> >>I think somewhere I have in my overloaded filing cabinets an article
> >> >>from a learned aerospace journal which deals with induced drag for
> >> >>wings operating in three dimensions.  My recollection (unchecked
> >> >>because the article is somewhere misplaced) was that when the wing
> >> >>was considered to operate in three dimensions, and computing power
> >> >>was brought to bear on the calculations, a slender wing with the
> >> >>outer sections bending upwards and backwards could achieve an
> >> >>induced drag coefficient BELOW the minimum as determined from two
> >> >>dimensional aerodynamics.
> >> >>
> >> >>I remember when the Nimbus 4 first came out and there was a photo of
> >> >>the 25 m wings bending significantly upwards during steep
> >> >>thermalling turning.  So we have with our sailplanes with higher
> >> >>aspect ratios and more slender spars wings which are operating in
> >> >>three dimensions.
> >> >>
> >> >>So I do not think that wing kinks in the outer wing panels are a
> >> >>fashion statement or a marketing ploy, but rather founded on serious
> >> >>efforts to reduce drag.
> >> >>
> >> >>Beyond that I leave it to some far more knowledgeable person on wing
> >> >>aerodynamics to provide futher illumination on the matter.
> >> >>
> >> >>Cheers
> >> >>
> >> >>Roger Druce
> >> >>
> >> >><mailto:[EMAIL PROTECTED]>[EMAIL PROTECTED]
> >> >>
> >> >>
> >> >
> >> > Roger,
> >> >
> >> > I think I have the same article by the late R.T.Jones of NACA and
> >> > later NASA reknown. I guess the issue is - does the discontinuity at
> >> > the kink increase the profile drag more than the 3D nature of the
> >> > bent wing decreases it.
> >> >
> >> > The tendency at a kink is for the leading edge discontinuity to trip
> >> > flow to turbulent and for the airfoil to stall earlier    although it
> >> > would seem you would need a fairly marked kink for this to occur.
> >> > Allegedly this is what happened on the F4U Corsair(the earlier stall
> >> > in the kink.
> >> >
> >> > Mike
> >> > Borgelt Instruments - manufacturers of quality soaring instruments
> >> > phone Int'l + 61 746 355784
> >> > fax   Int'l + 61 746 358796
> >> > cellphone Int'l + 61 428 355784
> >> >           Int'l + 61 429 355784
> >> > email:   [EMAIL PROTECTED]
> >> > website: www.borgeltinstruments.com
> >> >
> >> > _______________________________________________
> >> > Aus-soaring mailing list
> >> > [email protected]
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> >> >
> >> >
> >> >
> >> >
> >> > _______________________________________________
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> >> >
> >> > -- 
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> > 19/06/2006
> >> >
> >> >
> >>
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