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Title: TEXCAD: TEXile Composite Analysis for Design

Conference ·
OSTI ID:188457

The Textile Composite Analysis for Design (TEXCAD) code provides the materials/design engineer with a user-friendly, desktop computer based tool for the analysis of a wide variety of fabric reinforced woven and braided composites. It can be used to calculate overall thermal and mechanical properties along with engineering estimates of damage progression and strength. TEXCAD also calculates laminate properties for stacked, oriented fabric constructions. It discretely models the yarn centerline paths within the textile repeating unit cell (RUC) by assuming sinusoidal undulations at yarn cross-over points and uses a year discretization scheme (which subdivides each yarn into smaller, piecewise straight yarn slices) together with a 3-D stress averaging procedure to compute overall stiffness properties. In the calculations for strength, it uses a curved beam-on-elastic foundation model for yarn undulating regions together with incremental approach in which stiffness properties for the failed yarn slices are reduced based on the predicted yarn slice failure mode. Nonlinear shear effects and nonlinear geometric effects can be stimulated. Input to TEXCAD consists of: (1) material parameters like impregnated yarn and resin properties such as moduli, Poisson`s ratios, coefficients of thermal expansion, nonlinear shear parameters, axial failure strains, and in-plane failure stresses; and (2) fabric parameters like yarn sizes, braid angle, yarn packing density, filament diameter, and overall fiber volume fraction. Output consists of overall thermoelastic constants, yarn slice strains/stresses, yarn slice failure history, in-plane strain response, and ultimate failure strength. Strength can be computed under the combined action of thermal and mechanical loading (tension, compression, and shear). A brief overview of the analytical capabilities, program organization, and modules, input and output parameters of the TEXCAD code are presented here.

Research Organization:
NASA Langley Research Center, Hampton, VA (United States)
OSTI ID:
188457
Report Number(s):
N-96-17705; NASA-CP-3311-PT-2; NAS-1.55:3311-PT-2; L-17532B; NIPS-96-06187; CONF-9412106-; CNN: NAS1-19399; NAS1-19708; TRN: 9617717
Resource Relation:
Conference: Mechanics of textile composites conference, Hampton, VA (United States), 6-8 Dec 1994; Other Information: PBD: Oct 1995; Related Information: Is Part Of Mechanics of Textile Composites Conference; Poe, C.C.; Harris, C.E.; PB: 433 p.
Country of Publication:
United States
Language:
English

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