This design is due to Mr. B.I. Cheranovski.
The model of that device was from the experimental aerodynamic central institute in Moscow [TsAGI]; it has the original provision that appears in the picture.
The very wide wing surface has the special shape seems that the conditions of static and dynamic stability are favourable, even in respect to the moments around the three axes, the vertical axis, longitudinal and transverse. The experimental [parabola wing] system was already use in the development of glider aircraft models.
The parabolic wing was equipped with two engines (75 hp each) with symmetrical propellers. The wing was extended 12 metres, its maximum depth of 4.5 metres; wing area 25 sq m. Total weight including the engines was 1,200 kg with a maximum speed of 120 km/h.