Design procedures for fiber composite structural components : Panels subjected to combined in-plane loads
- Chamis, C. C.
- JAN 1, 1985.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- Step by step procedures are described which can be used to design panels made from fiber composite angleplied laminates and subjected to combined in plane loads. The procedures are set up as a multistep sample design. Steps in the sample design procedure range from selection of the laminate configuration to the subsequent analyses required to check design requirements for: (1) displacement, (2) ply stresses, and (3) buckling. The sample design steps are supplemented with appropriate tabular and graphical data which can be used to expedite the design process.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19850007514., Accession ID: 85N15823., NASA-TM-86909., E-2319., NAS 1.15:86909., and Ann. Conf. of the Society of the Plastics Industry (SPI) Reinforced Plastics/Composites Inst.,; 28 Jan. - 1 Feb. 1985; Atlanta, GA; United States.
- No Copyright.
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