There has long been a suspicion that a high wing location would be better to get a better lift distribution across the span.

Putting a wing on a pylon above the fuselage still gives you 4 intersections and the drag of the pylon.

The problem with the high wing is the lower intersection of the wing root with the fuselage and the interaction of the leading edge of the wing with the fuselage. Note the JS3 in that area also. Re-entrant intersections are particularly bad and as I noted, in the past

the CFD tools have not been available to quickly determine promising shapes.

The Mu 31 attempts to overcome this by careful shaping in the underwing/fuselage junction and leading edge, lots of CFD and wind tunnel testing and getting only 2 intersections instead of 4 Nowadays wind tunnels in the subsonic turbulent flow regime are used to

verify the CFD results and are very successful.

It was smart to base this heavily on the ASW27 as it should take all of an hour or so to do a comparison glide with an ASW27 at the same wing loading after a dual tow to 10,000 feet, at least as a first cut. It has been in development for 10 years. Note Jonkers

have their own Akaflieg in the pool of engineering students at Northwestern University.

I've seen a paper on the web on the Mu 31 design with CFD results, flow tests etc. IIRC they are talking 6 to 10% improvement depending on speed. If it really gets half that, expect to see some changes in new designs or modifications of old ones particularly if the

JS3 is shown to go well. Not a given when it gets down to survival conditions although it will go well on good days. The hit rate on successful competition gliders designed to be such isn't anywhere near 100%.

Mike


 At 08:20 AM 12/29/2017, you wrote:
Hi Ross

Whether it is a good idea or not remains to be seen.

Please keep in mind that the Mü 31 is only a student research project. Its existence should not be seen as an indication that a high wing design is beneficial in terms of performance. In fact there are very significant aerodynamic disadvantages with this concept and one of them is the huge amount of parasite drag on the underside of the wing/fuselage junction. There are others too, and it is high noon that this hype comes down to a more rational level.

Please don’t think for a moment that the move away from the early high wing designs on composite gliders wasn’t made
for very good reasons.

Kind regards

Bernard

On 29 Dec 2017, at 8:16 am, Ross McLean <<mailto:[email protected]>[email protected]> wrote:

And yet the European manufacturers have ignored their own research for so many years. It took the South African Jonkers brothers to put it into production again with their outstanding 15m/18m JS3 Rapture.
Now suddenly the Akaflieg have realised it was a good idea after all.
ROSS
_________________________________________________________________________________________
 Ross McLean
 Mobile:           + 61 488 270 105
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From: Aus-soaring [<mailto:[email protected]>mailto:[email protected]] On Behalf Of Peter Champness
Sent: Thursday, 28 December 2017 5:37 PM
To: Discussion of issues relating to Soaring in Australia.
Subject: Re: [Aus-soaring] ASG29R

I attended a talk by Gerhard Waibel about 10 years ago (or maybe 15 years ago).

Among other things he talked about the wing fuselage intersection drag. His idea was to raise the wing on a thin pylon more than 200mm above the fuselage and then support the wing with struts! I thought that was really reinventing the wheel. But he was right. Here we go.

On Thu, Dec 28, 2017 at 8:22 AM, Mike Borgelt <<mailto:[email protected]>[email protected]> wrote: Yes, as Bernard said there are other composite sailplanes with high wings. Phoebus C, Std Jantar 2/3, ASW 15.

However have another look at the Mu 31, the fuselage cross section in particular where at around pilot shoulder height it necks in. This is more like the Weihe, Meise (Olympia), Slingsby Sky, early Slingsby Skylarks etc.

Mike







the At 01:08 PM 12/27/2017, you wrote:

Not just new wings (same sections though ) but extensive changes to fuselage also so I think a new model number is warranted. Better for sales anyway. Wouldn't surprise me if the EB29R is further modified and becomes the EB30. Looking at the R wing at Benalla it didn't really fit the old root fairings on the EB29.

Funny thing is some of the wooden gliders of the 30s, 40s and 50s had similar wing locations and mounting of the wings on a pylon integrated into the fuselage. Didn't have the fancy wing root design as they didn't have the CFD codes or computers then.

Somewhere I have a paper on the Mu31 where they say they hope to get 6 to 10% drag reduction with the wing location. We should know soon as it won't be hard to find a good ASW27 and do comparison flights.

Before anyone gets too excited this is all pure speculation on my part but if the comparison tests show they are getting what they wanted........

Mike




At 12:43 PM 12/27/2017, you wrote:

Content-Language: en-US
Content-Type: multipart/alternative;

boundary="_000_PS1PR04MB1004D9231BF7DE336AFA7056A2070PS1PR04MB1004apcp_"

Hearing that this will be the glider that combats the V3 & JS3; new wings for the very popular ASG29, the R is for Racing - perhaps a play on the intimidating EB29R?





"ROCKS" ?
Looks like Butch had a good time in the V2 aswell.
Jim





what does that mean??
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