A composite laminated plate comprising a first plurality of plies of reinforcing fibers for lengthwise strength with respect to a dominant load direction, and a second plurality of reinforcing fibers oriented at angles ±β with respect to the dominant load direction, where β is between 15 and 35 degrees.
COMPOSITE LAMINATED PLATE HAVING REDUCED CROSSPLY ANGLE
2016-01-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / E04C STRUCTURAL ELEMENTS , Bauelemente |
Postbuckling analysis of crossply laminated plates
AIAA | 1975
|COMPOSITE LAMINATED PANEL WITH REDUCED ANGLE OF CROSS PLIES
European Patent Office | 2018
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