Abstract
Woven-roving and stitch-bonded composites were studied under low velocity impact loads. A woven structure, composed of roving, which is a collection of glass filaments put together, is known as woven-roving structure, whearas stitch-bonded fabric structure is produced mechanically combining the warp (0°) and weft (90°) roving. The FGI 1800 A2 E-Glass stitch bonded fabric and FGI 1854 E-glass woven-roving fabric both manufactured by Fiber Glass Industries were used for the study. A three dimensional mosaic finite element model of woven roving composite was developed to predict the quasi-static response stimulating the low velocity impact.
| Original language | English |
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| Title of host publication | Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference |
| Place of Publication | usa |
| Pages | 4405-4415 |
| Number of pages | 11 |
| Volume | 6 |
| State | Published - Dec 1 2004 |
| Event | Collect. of Pap. - 45th AIAA/ASME/ASCE/AHS/ASC Struct., Struct. Dyn. and Mater. Conf.; 12th AIAA/ASME/AHS Adapt. Struct. Conf.; 6th AIAA Non-Deterministic Approaches Forum; 5th AIAA Gossamer Spacecraft Forum - Palm Springs, CA, United States Duration: Apr 19 2004 → Apr 22 2004 |
Conference
| Conference | Collect. of Pap. - 45th AIAA/ASME/ASCE/AHS/ASC Struct., Struct. Dyn. and Mater. Conf.; 12th AIAA/ASME/AHS Adapt. Struct. Conf.; 6th AIAA Non-Deterministic Approaches Forum; 5th AIAA Gossamer Spacecraft Forum |
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| Country/Territory | United States |
| City | Palm Springs, CA |
| Period | 04/19/04 → 04/22/04 |