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Am Samstag, 21. November 2015 00:11:10 UTC+1 schrieb Eric Greenwell:
Tango Whisky wrote on 10/28/2015 11:15 AM: I haven't done this, but my former TW (SN 360) had received a C-fuselage when it was owned by Martin Heide, and I had bought it like this. Schleicher has issued a technical note on this (it's an approved modification), so best would be to talk to them. You'll get the best of two world's - the advantages of the C fuse, and the 55 deg flaps. The C wins offer no advantage whatsoever. I had a C model for 11 years, and was under the impression the wings were slightly different from the "A" wings, mainly to improve resistance to spinning. How would the C fuselage provide 55 degree flaps? I think the mechanism is all in the fuselage, not in the wings. -- Eric Greenwell - Washington State, USA (change ".netto" to ".us" to email me) - "A Guide to Self-Launching Sailplane Operation" https://sites.google.com/site/motorg...ad-the-guide-1 - "Transponders in Sailplanes - Dec 2014a" also ADS-B, PCAS, Flarm http://soaringsafety.org/prevention/...anes-2014A.pdf Well, I don't know how it is done in detail, but my ASW20 had a C-fuselage, the A-wings and 55 deg flaps. I guess that you can adjust the mixer to give 55 deg on the flaps. The C-wings have no advantage whatsoever, and they are certainly not more spin resistent. I have flown an ASW20C with CG near the aft limit, and it was a bitch. |
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On Monday, November 23, 2015 at 2:53:33 AM UTC-5, Tango Whisky wrote:
Am Samstag, 21. November 2015 00:11:10 UTC+1 schrieb Eric Greenwell: Tango Whisky wrote on 10/28/2015 11:15 AM: I haven't done this, but my former TW (SN 360) had received a C-fuselage when it was owned by Martin Heide, and I had bought it like this. Schleicher has issued a technical note on this (it's an approved modification), so best would be to talk to them. You'll get the best of two world's - the advantages of the C fuse, and the 55 deg flaps. The C wins offer no advantage whatsoever. I had a C model for 11 years, and was under the impression the wings were slightly different from the "A" wings, mainly to improve resistance to spinning. How would the C fuselage provide 55 degree flaps? I think the mechanism is all in the fuselage, not in the wings. -- Eric Greenwell - Washington State, USA (change ".netto" to ".us" to email me) - "A Guide to Self-Launching Sailplane Operation" https://sites.google.com/site/motorg...ad-the-guide-1 - "Transponders in Sailplanes - Dec 2014a" also ADS-B, PCAS, Flarm http://soaringsafety.org/prevention/...anes-2014A.pdf Well, I don't know how it is done in detail, but my ASW20 had a C-fuselage, the A-wings and 55 deg flaps. I guess that you can adjust the mixer to give 55 deg on the flaps. The C-wings have no advantage whatsoever, and they are certainly not more spin resistent. I have flown an ASW20C with CG near the aft limit, and it was a bitch. C is slightly better at high speed from my experience. I owned both and test flew them against each other. UH |
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