Pt B, Ch 12, Sec 3The contents in mass are obtained from the following formulae:• M f = fibres’ mass (gr/m 2 )/individual layer’s mass (gr/m 2 )• M m = resin’s mass (gr/m 2 )/individual layer’s mass (gr/m 2 )• V f and V m are defined in [1.1.3].V f =( M f ⁄ ρ f )-------------------------------------------------------------( M f ⁄ ρ f ) + (( 1 – M f ) ⁄ ρ m )V m = 1 – V fM f =( V f × ρ f )---------------------------------------------------------------( V f × ρ f ) + (( 1 – V f ) × ρ m )M m = 1 – M fwith all parameters defined in [1.1.3].2.1.2 The resin/fibre mix ratio is to be specified by the shipyardand depends on the laminating process.For information only, the common ratio values are given inTab 1.2.2 Individual layer’s thickness2.2.1 The individual layer’s thickness, in mm, can beexpressed from the fibre’s content, in mass or in volume, bythe following formulae:⎛ 1 1 – MP f ⋅ ⎛---+ ---------------- f ⎞⎞⎝ ⎝ρ f M f ⋅ ρ m⎠⎠e = ------------------------------------------------1000Pe f ⁄ ( V f ⋅ ρ f )= --------------------------1000with all parameters defined in [1.1.3].2.3 Mass, voluminal mass and density of anindividual layer2.3.1 The density of an individual layer is obtained by thefollowing formula:ρ = ρ f × V f + ρ m × ( 1 – V f )with all parameters defined in [1.1.3].3 Elastic coefficient of an individual layer3.1 Unidirectionals3.1.1 Reference axisThe reference axis system for a unidirectional is as follows(see Fig 1):• 1 : axis parallel to the fibre’s direction• 2 : axis perpendicular to the fibre’s direction• 3 : axis normal to plane containing axis 1 and 2, leadingto direct reference axis system.The reference axis for an elementary fibre is defined as follows(see Fig 2):• 0° : Longitudinal axis of the fibre• 90° : Transverse axis of the fibre.Figure 1 : Reference axis for unidirectionalsFigure 2 : Reference axis of an elementary fibre0°3.1.2 Elastic coefficientsThe elastic coefficients of an unidirectional are estimated bythe following formulae, with all parameters defined in[1.1.3]:• Longitudinal Young’s modulus E UD1 , in MPa:E UD1 = C UD1 × ( E f0° × V f + E m × ( 1 – V f ))• Transverse Young’s moduli E UD2 and E UD3 , in MPa:⎛⎞2⎜ EE UD2 E UD3 C ⎛ mUD2-------------- ⎞ 1 + 0,85 ⋅ V f⎟= = × ⎜ × ----------------------------------------------------------------⎝ 21 – ν ⎠⎟⎜ m( 1 – V f ) 1,25 E--------- m V+ × -------------- f ⎟⎝2E f90° 1 – ν ⎠m• Shear moduli, in MPa:1 + η ⋅ VG UD12 = G UD13 = C UD12 ⋅ G × ---------------------- fm1 – η ⋅ V fwith⎛-------⎞ – 1⎝G m⎠η = ----------------------⎛ G------- f ⎞ + 1⎝ ⎠G UD23 = 0, 7 ⋅ G UD12• Poisson’s coefficients:ν UD13 = ν UD12 = C UDν × ( ν f × V f + ν m × ( 1 – V f ))G fG mEν UD21 = ν UD31 = ν UD2UD12 × ----------E UD1The coefficients C UD1 , C UD2 , C UD12 and C UDν areexperimental coefficients taking into account the specificcharacteristics of fibre’s type. They are given in Tab 2.!90°′ν UD23 = ν UD32 = C UDν × ( ν f × V f + ν m × ( 1 – V f ))′ Ewith ν f = νf90°f ⋅ ---------E f0°July 2006 with February 2008 Amendments Bureau Veritas Rules for Yachts 289
Pt B, Ch 12, Sec 3Table 1 : Resin / fibre mix ratios (in %)Laminating Process V fM fGlass Carbon Para-aramidMat from 15 to 20 from 25 to 35 - -Hand Lay-upRoving from 25 to 40 from 40 to 60 from 35 to 50 from 30 to 45Unidirectional from 40 to 50 from 60 to 70 from 50 to 60 from 45 to 55Infusion 45 60 55 50Pre-pregs from 55 to 60 from 60 to 70 from 65 to 70 from 60 to 65Table 2 : Coefficients C UD1 , C UD2 , C UD12 and C UDν3.2 Woven Rovings3.2.1 Reference axisThe reference axis defined for woven rovings are the samethan for unidirectionals with the following denomination:• 1 : axis parallel to warp direction• 2 : axis parallel to weft direction• 3 : axis normal to plane containing axis 1 and 2, leadingto direct reference axis system.3.2.2 Woven balance coefficient C eqThe woven balance coefficient is equal to the mass ratio ofdry reinforcement in warp direction to the total dry reinforcementof woven fabric.3.2.3 Elastic coefficientsThe elastic coefficients of woven rovings as individual layersare estimated by the following formulae:• Young’s modulus in warp direction E T1 , in MPa:• Young’s modulus in weft direction E T2 , in MPa:• Out-of-plane Young’s modulus E T3 , in MPa:E T3 = E UD3E-glass R-GlassCarbonHSCarbonIM• Shear moduli G 12 , G 23 and G 13 , in MPa:CarbonHMParaaramidC UD1 1 0,9 1 0,85 0,9 0,95C UD2 0,8 1,2 0,7 0,8 0,85 0,9C UD12 0,9 1,2 0,9 0,9 1 0,55C UDν 0,9 0,9 0,8 0,75 0,7 0,91 AE T1 = -- ⋅ ⎛A 12e11 – ------- ⎞⎝ ⎠2A 221 AE T2 = -- ⋅ ⎛A 12e22 – ------- ⎞⎝ ⎠2A 111G T12 = -- ⋅ Ae33 and G T23 = G T13 = 0, 9 ⋅ G T12• Poisson’s coefficients:Aν 12T12 = -------where:with:A 22Eν T21 = νT2T12 ⋅ ------Note 1: Parameters with suffix UD are defined in [3.1].3.3 Chopped Strand Mats3.3.1 GeneralE T1ν T32 = ν T31 = ( ν UD32 + ν UD31 ) ⁄ 2ν T13 = ( ν UD23 + ν UD13 ) ⁄ 2A 11 = e ⋅ ( C eq ⋅ Q11 + ( 1 – C eq ) ⋅ Q 22 )A 22 = e ⋅ ( C eq ⋅ Q 22 + ( 1 – C eq ) ⋅ Q 11 )A 12 = e ⋅ Q 12A 33 = e ⋅ Q 33Q 11 = E UD1 ⁄ ( 1 – ( ν UD12 ⋅ ν UD21 ))Q 22 = E UD2 ⁄ ( 1 – ( ν UD12 ⋅ ν UD21 ))Q 12 = ( ν UD21 ⋅ E UD1 ) ⁄ ( 1 – ( ν UD12 ⋅ ν UD21 ))=Q 33G UD12A chopped strand mat is made of cut fibres, randomarranged and supposed uniformly distributed in space. It isassumed as isotropic material.3.3.2 Elastic coefficientsIsotropic assumption makes possible to define only threeelastic coefficients obtained by the following formulae:• Young’s moduli, in MPa:3 5E mat1 = E mat2 = -- ⋅ E8UD1 + -- ⋅ E8UD2=E mat3E UD3• Poisson’s coefficient is as all isotropic materials:ν mat12 = ν mat21 = ν mat32 = ν mat13 = 0,3• Shear moduli, in MPa:G mat12 = E mat1 ⁄ ( 2 ⋅ ( 1 + ν mat21 ))G mat23 = G mat31 = 0, 7 ⋅ G UD12Where parameter with suffix UD are defined in [3.1].Note 1: Parameters with suffix UD are defined in [3.1].290 Bureau Veritas Rules for Yachts July 2006 with February 2008 Amendments
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