Wavy flying-wing aircraft pressure chamber

The invention belongs to a flying-wing aircraft design technology, and in particular relates to a wavy flying-wing aircraft pressure chamber. The number of upper skins of the wavy flying-wing aircraft pressure chamber is equal to that of lower skins; the upper skins and the lower skins are shaped like longitudinal waves in position corresponding to each other; the longitudinal wavy parts of the upper and lower skins extend from the leading edge of a wing to the trailing edge of the wing, and the transverse spans are basically the same. According to the wavy flying-wing aircraft pressure chamber, by designing the wavy parts on the surfaces of the upper and lower skins, the surface of the pressure chamber is circular or approximately circular, so that membrane stress is mainly applied to the skins of the pressure chamber through a differential pressure load, and the defect of large tension stress caused by applying of bending moment to straight wing skins through the differential pressure load is overcome. Therefore, the wavy flying-wing aircraft pressure chamber has the characteristics that the differential pressure load bearing capacity of the pressure chamber can be improved; the structure design, the weight control, the manufacturing, the maintenance and the like are further facilitated.