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Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets
U.S. Government
Paperback. Books LLC, Reference Series 2012-06-23.
ISBN 9781234283469
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Förlagets beskrivning
Original publisher: Hampton, Va. : Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997] OCLC Number: (OCoLC)46708482 Subject: Composite materials. Excerpt: ... Table I. Details of facesheet laminate ply stacking sequences. Laminate 1 ( 50 plies )-Thickest laminate [ ± 45 / 0 / + 45 / 90 / 0 / ? 45 / 0 / + 45 / 90 / 0 / ? 45 / 90 / 0 / ± 45 / 0 / ? 45 / 90 / 0 / + 45 / 0 / ± 45 / 0 ] s Laminate 2 ( 48 plies ) [ ± 45 / 0 / + 45 / 90 / 0 / ? 45 / 0 / + 45 / 90 / 0 / ? 45 / 90 / 0 / + 45 / 0 / ? 45 / 90 / 0 / + 45 / 0 / ± 45 / 0 ] s Laminate 3 ( 46 plies ) [ ± 45 / 0 / + 45 / 90 / 0 / ? 45 / 0 / + 45 / 90 / 0 / ? 45 / 90 / + 45 / 0 / ? 45 / 90 / 0 / + 45 / 0 / ± 45 / 0 ] s Laminate 4 ( 43 plies ) [ ± 45 / 0 / + 45 / 90 / 0 / ? 45 / 0 / + 45 / 90 / 0 / ? 45 / 90 / + 45 / 0 / ? 45 / 90 / 0 / + 45 / 0 / + 45 / 0 / 2 ? 45 / 0 / + 45 / 0 / 90 / ? 45 / 0 / + 45 / 90 / ? 45 / 0 / + 45 / 0 / ? 45 / 0 / 90 / + 45 / 0 / m 45 ] Laminate 5 ( 41 plies ) [ ± 45 / 0 / + 45 / 90 / ? 45 / 0 / + 45 / 90 / 0 / ? 45 / 90 / + 45 / 0 / ? 45 / 90 / 0 / + 45 / 0 / + 45 / 0 / ? 45 / 0 / 2 + 45 / 0 / 90 / ? 45 / 0 / + 45 / 90 / ? 45 / 0 / + 45 / 0 / ? 45 / 90 / + 45 / 0 / m 45 ] Laminate 6 ( 40 plies ) [ ± 45 / 0 / + 45 / 90 / ? 45 / 0 / + 45 / 0 / ? 45 / 90 / + 45 / 0 / ? 45 / 90 / 0 / + 45 / 0 / + 45 / 0 / 2 ? 45 / 0 / + 45 / 0 / 90 / ? 45 / 0 / + 45 / 90 / ? 45 / 0 / + 45 / 0 / ? 45 / 90 / + 45 / 0 / m 45 ] Laminate 7 ( 38 plies ) [ ± 45 / 0 / + 45 / 90 / ? 45 / 0 / ? 45 / 90 / + 45 / 0 / ? 45 / 90 / 0 / + 45 / 0 / + 45 / 0 / 2 2 ? 45 / 0 / + 45 / 0 / 90 / ? 45 / 0 / + 45 / 90 / ? 45 / 0 / ? 45 / 90 / + 45 / 0 / m 45 ] 2 Laminate 8 ( 36 plies )-Thinnest laminate 45 0 45 90 45 0 45 90 45 0 45 0 45 0 45 90 ) [ ± / / + / / ? / / ? / / + / / + / / ? / / + / / ( ) ( 2 2 2 2 ? 45 0 ? 45 90 + 45 0 m 45 ] / / / / / / 2 14
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Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets
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