Schleicher ASW 20

The ASW 20 is constructed from glass-reinforced plastic. It features trailing edge flaps which interconnect with the ailerons and allow the entire trailing edge to operate as a flap between -9 and +5 degrees. The flaps also act as ailerons, but deflect only half of the aileron amount. Schempp-Hirth type airbrakes are provided on the upper wing surface. The B model (introduced in 1983) differs from the A and C model in that it uses a reinforced wing spar, which provides an increased water ballast capacity at the expense of the flexible wing. The B and C model include several enhancements over the original A model, including a lifting panel, hydraulic disc brake, and automatic elevator hookup. The B and C wings also incorporate a pneumatic turbulator system, which draws high pressure air from pitot inlets on the wing and injects it through approximately 860 pinholes into the boundary layer to control underwing airflow separation. ASW 20s that include a L designation may be fitted with a 1.59 m wingtip extension. The F designation was assigned to A variants produced in France by Centrair. Centrair also produced an FL variant equivalent to the German ASW20L; most of these are only permitted to fly without the wingtip extensions due to a deficiency in the wing spar construction. At least three different winglet designs have been produced for the ASW 20, including a NASA winglet fitted to the Centrair gliders (FP), a design by Peter Masak, and a second generation winglet designed by Prof. Mark D. Maughmer of Penn State University(USA). ==Flight characteristics==

The ASW-20 is known as a very pleasant handling glider in most respects. The wing structure composite layup was designed to twist slightly as the wings flexed upward, resulting in the ability to "store" some of the energy from atmospheric gusts, and then release that energy with a very slight forward thrust force as the wings flexed back downward to their normal position. This concept is known as the Katzmayr Effect, and somewhat mimics a bird's ability to use a flapping motion to propel itself forward in flight. This unique wing twisting movement gave the ASW-20 an ability to make very small but consistent performance gains (or reduced losses) in turbulent and gusty thermal conditions compared to other competition level sailplanes. The landing flaps (55° in early models, 38° in later models), in conjunction with very effective airbrakes, allow the pilot to make exceptionally steep approaches at slow speeds, permitting very short landings when required. Second generation winglets further improved the handling and reduced drag at low to mid speeds. Thermal performance is comparable to gliders of more modern eras. These characteristics have made the ASW-20 a much beloved and desirable aircraft, even after it was no longer competitive in racing. One very common modification was the insertion of an intermediate flap setting detent (between zero and +1 position) which mitigated or softened any "tip-stall" and associated risk of spinning while thermaling in tight, gusty thermals. The flexible wing of the A and C models is particularly favored for ridge running, where it absorbs some of the tremendous turbulence found at ridgetop. ==Variants==

;ASW20: Prototype and initial production ;ASW20L:the ASW20 with detachable outer wing extensions to span, to compete in the Open-class. ;ASW20B: ;ASW20BL:the ASW20B with detachable outer wing extensions to span, to compete in the Open-class. ;ASW20C: ;ASW20CL:the ASW20C with detachable outer wing extensions to span, to compete in the Open-class. ;ASW20CLT: Open-class glider with PSR T01 turbojet sustainer ;ASW20F: ASW20A produced in France by Centrair ;ASW20FP: The ASW20F with NASA winglets designed to improve performance in weak conditions. ;Z-20: Brazilian Air Force designation of the ASW 20. ==Specifications (ASW 20B)==