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In science, extraordinary claims require extraordinary proof. On older designs, we have the published Dick Johnson's reports. While his methodology was not problem free, it was objective, independent, consistent, repeatable, and fully documented.
On Wednesday, October 7, 2020 at 10:30:06 PM UTC-7, Paul T wrote: At 04:12 08 October 2020, 2G wrote: On Tuesday, October 6, 2020 at 1:58:06 PM UTC-7, Eric Greenwell wrote: The JS website says it's 60 for the JS1C/21M; 63 for the JS2/21M. jfitch wrote on 10/6/2020 1:37 PM: Link? Google produces zero results. On Tuesday, October 6, 2020 at 1 1:00:06 AM UTC-7, Paul T wrote: At 15:39 06 October 2020, jfitch wrote: They are claiming 63:1, that is 7 points higher than AS claim of 56:1. I th= ink it is best explained by a mistake in their math. I'd be interested in s= eeing the test data proving it.=20 On Tuesday, October 6, 2020 at 12:53:25 AM UTC-7, Carlo Orsini wrote: Thank you for your first hand infos, those are good news for me (I don't = understand why they advertise these dimensions in a different way). JS2 see= ms to be a nice project overall. Hard to me to understand where they strech= ed out those +4 points of efficency in 21m, according to their calculated p= olars, compared to ASH31 (yes I know that '31 profiles are a bit superseede= d and the aspect ratio is a factor too but 4 points are a huge amount!!). Those two dimensions for the JS2 and the ASH31 are clearly not be compa= rable - one internal cockpit rim and one external I guess. The 525mm should= er width for the JS2 is exactly the same as the quoted figure for the JS1 (= and JS3) and the JS1 cockpit roominess is fully equal to the ASH26/31 from = which it was derived. I have 4 years in a JS1 followed by 2 in the ASH 26e = and they are so similar that it would be hard to know which cockpit I was i= n with my eyes closed. Looking at the JS2 cockpit photographs it obvious th= at its structural cockpit rim design is the same as the 31, 26 and JS1. JS = do not make small cockpits. I believe the Idafleig measured a JS1C at 63:1......so the JS2 witH its few improvements on the JS1C should achieve that.... -- Eric Greenwell - Washington State, USA (change ".netto" to ".us" to me) - "A Guide to Self-Launching Sailplane Operation" https://sites.google.com/site/motorg.../download-the- guide-1 Someone might ask them how they came up with these L/D figures because I understand that they aren't from actual flight tests. Tom THE JS1C TO MY KNOWLEDGE HAS BEEN MEASURED AT 63:1 BY THE IDAFLEIG IN ITS FLIGHT TESTS- PROBABLY THE MOST RELIABLE WAY OF MEASURING A GLIDERS POLAR. (I THINK THE JONKERS BOYS WHERE SUPRISED BY THAT FIGURE AS IT IS RARE FOR A GLIDER TO EXCEED ITS THEOROTICAL FIGURE -BUT IT DOES HAPPEN.) ALL MANUFACTURERS FIGURES ARE AT BEST 'THEORETICAL' UNTIL MEASURED.................. SOME ARE WILDLY OPTIMISTIC - BUT BEST L/D DOESNT MEAN MUCH THESE DAYS REALLY................. ITS NOT AS THOUFGH THIS AIRCRAFT AS NOT PROVED ITSELF IN THE CONTEST ARENA IS IT....... |
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