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At 16:18 21 February 2016, Dan Daly wrote:
On Saturday, February 20, 2016 at 1:23:11 PM UTC-5, wrote: Anything interesting to report from Christoph Wannemacher's presentation = on "Design Philosophy for the New Ventus" e.g information on the aspect rat= io, aerofoil, wing thickness, transition position, turbulators etc? =20 John Galloway From my notes: 600kg 10.83 m2/116.575 sq ft 55.4 kg/m2 11.35 psf AR 29.9 sport (little - 2cxa size - based on 2cxa) side-hinged canopy Goal of certification and having a number available for WGC Bennala down the road, FES and T then performance edition (larger) quintus cockpit self-launch (T or FES if demanded... but SL first) Description of new wx model; validation using WGC Uvalde data and Euro cham= pionship. Result - you have 2 modes, thermalling or fast and spend almost = no time at best L/D. goal to optimize for these 2 modes. climb perf in weak small thermals - data from euro contests - lift that V2C= XT couldn't climb in, V3 had theoretical 15 kph x-c speed (contests are won= or lost on the weakest days). Goal of increased cross-country speed. Started with an aero check of Arcus from large contests to validate that ae= rofoil. Result - good basis for start of work on V3 ("new Ventus" accordin= g to S-H marketing but informally known as V3). General of description of wing evolution from original Discus to this; disc= ussion of winglets too (didn't take notes) wing thickness root 14.8% closing in to root 12.9% outboard of spoiler box 13.2% blend near winglet 13.1% Horizontal tail volume/area reduced Flutter - certification for CS22 AL2 - higher torsional stiffness Fuselage - higher crashworthiness =3D heavier fuselage 2 sets of water tanks (one small below bigger) - one release like zig-zag -= looks like you dump the big one but keep a smaller volume that doesn't slo= sh when you have partial water (not stated but that's what it looked like t= o me - I have been wrong on this kind of thing). Jan 29 first flight; to briefing date 20 flights / 13 hrs (wx has sucked in= Europe) Next, turbo in sport fuselage ~ 4-5 weeks. FES "in summer" In 6 weeks, mockup of big version; canopy to be forward-hinged carbon-fibre. "later" - solo 2625-01 injected SL system - better high and hot Questions - wing soft/stiff? Stiff. ran out of time for more... Overall, an impression of a fast-moving, ambitious programme that starts wi= th the pure gliders (small then big), and as resources permit, moving to tu= rbo, then SL, then FES (if there is demand). I think I have most of this correct - I was trying to pay attention and scr= ibble mostly legible notes. =20 If you have questions, best to ask the dealer... Thanks Dan. Very interesting. I asked the UK dealer for this type of information a couple of weeks ago but none was available then. JG |
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