AIAA-2006-1972 The application of residual stress tailoring of snap-through composites for variable sweep wings
47th, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference ; 2006 ; Newport, R.I
2006-01-01
12 pages
Paper numbers 2006-1600 to 2006-2284 with gaps held
Conference paper
English
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Tailoring Snap-through Loads in Variable Stiffness Composites (AIAA 2018-2245)
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