One embodiment includes a structural panel for an aerospace vehicle, including a single sheet of material, the material having a first raised pattern on a first side, and a second raised pattern on a reverse side, wherein a repeating portion of the first raised pattern is substantially identical in size and shape to a repeating portion of the second raised pattern, and is rotated at an angle θ to the first raised pattern.
ISOGRID PATTERNS FOR STRUCTURAL AIRCRAFT PANELS
2021-08-05
Patent
Electronic Resource
English
Warping of Flat Composite Isogrid Panels
British Library Conference Proceedings | 1997
|AIAA | 1975
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