Wing test piece and processing method thereof
A test piece and wing technology, which is applied in the field of aircraft wing performance testing, can solve the problems of high production cost and high wing stiffness, achieve high flexibility, meet the needs of large deformation, and low processing cost
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[0027] The technical solutions of the present application are clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present application. Apparently, the described embodiments are part of the embodiments of the present application, not all of them. Based on the embodiments in this application, all other embodiments obtained by those skilled in the art without making creative efforts belong to the scope of protection of this application.
[0028] refer to figure 1 , is a wing test piece disclosed in the embodiment of the present application, including a spar 1 , a rib 2 , a skin 3 and an airfoil foam 4 . In order to show the internal structure of the wing test piece more clearly, figure 1 Part of the skin3 was removed from one end of the
[0029] refer to figure 1 and figure 2 , the section of the spar 1 is I-shaped, which includes an upper edge plate 11, a lower edge plate 12 and a web 13, the upper edge plate 11 and...
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