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I have helped rig many sailplanes, both composite and conventional aluminum
construction. In almost every case the metal wing are lighter then the composite. (1-35 and HP-18 aluminum wings are lighter then ASW-20, ASW-27, and LS-6 composite wings.) It is much easier to build a laminar flow airfoil and complex shaped wing to fuselage transition using composite construction. These wing have a better lift to drag ratio. The decrease in drag aerodynamic drag of the wing and static drag decrease associated with the wing/fuselage transition allow faster speeds. Wayne http://www.soaridaho.com/ "cavelamb himself" wrote in message news ![]() At these speeds I suspect surface condition is a small part of the overall drag. However! If the new wing were a couple hundred pounds lighter, then you'd see some inprovement in speed. It takes power to stay aloft. The heavier the plane, the more power is required just to stay up. Lighter is mo' betta! Richard |
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