The truss-supported wing design has been studied by NASA and Boeing, with the design offering a high aspect ratio not unlike the wings of a glider. The obvious disadvantage of the long, narrow wings of a glider is that they are also long and fragile, which are not desirable characteristics on a commercial jetliner. By adding the truss bracing, the wing design can be optimized for high aspect ratio, while the fragility is compensated for by the spars. For a commercial jetliner, this can mean significantly less fuel consumption.
As (Think Flight) found, the typical problems with scaling wings up and down were also evident here, with the Reynolds number explaining the ‘why’ involving the chord length of the aerofoil, which is obviously different from a full-size jetliner and a model you can hold in your hand. Effectively, this means that on a model scale the effect of higher aspect ratio is not as pronounced as it is with jetliners, although the trusses may provide some advantage in structural stiffness.