Almost irreconcilable: best climbing performance, an excellent glide ratio - even at high speeds, optimal thermalling performance, and all in all very good-natured handling characteristics.
From wind tunnel to super-ellipse
These goals could be reached with the Antares. The aerodynamic design is the result of a multi-year research project. We have exploited all conceivable possibilities to optimize our glider, and designed it uncompromisingly all of a piece. We used and perfectly harmonized nine different wing airfoils to minimize drag. The laminar flow on the wing’s bottom surface reaches up to 95% of its depth. Zig-zag tape finally forces the laminar flow to transition to a turbulent boundary layer. According to investigations commissioned by Lange Aviation this method of influencing the boundary layer is not significantly different from installing suction openings – as long as you do correctly apply the tape to the predominant boundary layer. It is also less sensitive to dirt or damage. On the airfoil’s upper surface the circulating air stays laminar until having followed up to 75% of its depth. This currently represents the best indicated value for airfoils which do not utilize boundary layer suction technique. When flying at high speeds you can take advantage of an additional negative flap setting (- 3°). So, in the end you may fly at very high speeds and at the same time achieve a so far unreached gliding performance. Only at speeds over 220 km/h (119 kts) to 245 km/h (132 kts) (depending on your actual wing loading) these airfoils tend to fall out of the laminar flow.
An additional negative flap setting of -3° can be selected for fast glide. This allows for very high speed flights with unachievable glide performances. Only at air-speeds of 220 kph (119 kts) to 245 kph (132 kts) (depending on the wing loading), do the airfoils leave the laminar drag bucket.
The Antares 23’s wing geometry is described by an extremely slender super-ellipse. Thanks to this shape, the induced drag is reduced to its theoretical minimum. It corresponds to the ideal value of an untwisted and elliptical shaped wing, without having to fear critical stall characteristics of such a wing. The deep-gauged outer wings are responsible for good-natured flight qualities. Plus, our winglets reduce the induced drag by another 5%. <b>In total the 23 meter wingspan’s induced drag only measures 95% compared to an untwisted elliptic wing of similar span.</b>
Perfection to the finest detailThe Antares 23’s wing area is big enough and well dimensioned to meet a motor glider's requirements.
In combination with a high aspect ratio of 38.5 it guarantees superior climbing qualities at a minimized induced drag.
- Wings and winglets have been drafted in one unit. Perfectly matched with the wings our winglets thus significantly reduce drag and at the same time boost the flight qualities.
- The electric propulsion unit’s compact engine helps to realize an optimal contraction of the fuselage’s cross section which further reduces aerodynamic drag.
<b>When we at a later point introduced the sustainer engine we managed to integrate the entire engine installation without having to change the fuselage or the engine compartment's shape.</b>
- Common aerodynamic loss of performance in the wing-fuselage fillet is minimized by a specific layout of the fuselage section and through using particularly turbulent airfoils in the area close to the fuselage.