Braided and filament wound CFRP were fabricated with varied fiber orientations. These composites exhibited not only similar trends in their experimental strength and stiffness properties but also good correlations with predictions made by CLT.
CazeneuveCJoguetPMaileJCOytanaC. Predicting the mechanical behavior of Kevlar/Epoxy and carbon/epoxy filament wound tubes. Compos1992. 23(6): 415–424.
6.
SodenPDKitchingRTsePCTsavalasY. Influence of winding angle on the strength and deformation of filament-wound composite tubes subjected to uniaxial and biaxial loads. Compos Sci Technol1993. 46: 363–378.
7.
KaynakCErdillerESParnasSenelF. Use of split disk tests for the process parameters of filament wound epoxy composite tubes. Polym Test2005. 24(5): 648–655.
8.
PotluriPMananAFranckeMDayRJ. Flexural and torsional behaviour of biaxial and triaxial braided composite structures. Compos Struct2006. 75(1-4): 377–386.
9.
CharleboisKMBoukhiliRZebdiOTrochuFGasmiA. Evaluation of the physical and mechanical properties of braided fabrics and their composites. JReinf Plast Compos2005. 24(14): 1539–1554.
10.
CareyJMunroMFahimA. Regression based model for elastic constants of 2D braided/woven open mesh angle ply composites. Polym Compos2005. 26(2): 152–164.
11.
Oussama Zebdi, Rachid Boukhili and Francois Trochu. An inverse approach based on laminate theory to calculate the mechanical properties of braided composites. JReinf Plast Compos2009. 28(23): 2911–2930.
12.
LiXBiniendaWKGoldbergRK. Finite element model for failure study of two-dimensional triaxially braided composite2010. Cleveland, Ohio: NASA/TM-2010-216372, NASA Glenn Research Centre.
13.
ASTM D 3039 (Tensile), D 3410 (Compression) and D 3518 (In-plane shear) tests.
14.
Symposium on standards for filament wound reinforced plastics ASTM STP 327, Naval Ordnance Laboratory, White Oak, Silver spring, MD, June 6-7, 1962.
15.
YoonSHKimGChoWM. Measurement of tensile properties using filament wound ring specimens. J Reinf Plast Compos1997. 16(9): 810–824.
16.
Yeow-Cheong Ng. Deriving composite lamina properties from laminate properties using classical lamination theory and failure criteria. J Compos Mater2005. 39(14): 1295–1306.
17.
JonesRM. Mechanics of composite materials1999. 2nd ed. New York, USA: Taylor and Francis.
18.
Al-KhalilMFSSodenPD. Theoretical through thickness elastic constants for filament wound composite tubes. Int J Mech Sci1994. 36(1): 49–62.
19.
HyerMW. Stress analysis of fibre reinforced composite materials1998. New York, USA: WCB McGraw Hill Book Co.