This report is an archived publication and may contain dated technical, contact, and link information 

Publication Number: FHWAHRT04097
Date: August 2007 

Measured Variability Of Southern Yellow Pine  Manual for LSDYNA Wood Material Model 143PDF Version (2.92 MB)
PDF files can be viewed with the Acrobat® Reader® APPENDIX C. ANALYTICAL FORM OF CANDIDATE FAILURE CRITERIAC.1 REVIEW OF CRITERIANumerous failure criteria available in the literature were reviewed and evaluated for modeling the yield strength of wood and composite materials. To our knowledge, a validated threedimensional theory for modeling wood is not documented in the literature. However, numerous failure criteria have been documented for fiberreinforced plastic (FRP) composites (e.g., see the survey by Nahas^{(28)}). Composites are similar to wood because they are transversely isotropic materials with distinct failure modes in the parallel (fiber) and perpendicular (transverse fiber) directions. Therefore, many of the criteria originally developed for modeling composites were evaluated as candidates for modeling wood. The functional form of each failure criterion that was evaluated is given in section C.2. These include one limit and six interactive criteria. Both orthotropic and transversely isotropic criteria are reported. All criteria are stressbased criteria. The stresses are transformed to the principal material axes (LTR axes) before application of the failure criteria. Strainbased criteria were not evaluated because failure strains are not reported in the literature for wood. One cannot derive failure strains from stresses if the stressstrain behavior is nonlinear, as it is for wood in compression. A brief summary of each criterion is given here: Maximum Stress (commonly applied limit theory): Failure occurs when any component of stress exceeds its corresponding strength TsaiWu (tensor polynomial theory that was originally developed for anisotropic materials): It contains linear and quadratic stress terms. Seven coefficients must be defined for transversely isotropic applications. The noninteraction coefficients are determined from measured uniaxial and pure shear strengths. By noninteraction, one means terms that contain one component of stress (e.g., F_{1}s_{11}). The interaction terms are determined from measured biaxial strengths. By interaction, one means terms that have two or more components of stress multiplied together (e.g., F_{12}s_{11}s_{22}). Hoffman: Hoffman extended Hill’s distortional energy criterion for orthotropic materials to account for different strengths in tension and compression. The criterion contains linear and quadratic stress terms. Six coefficients are determined from uniaxial stress and pure shear tests. Biaxial strengths are not needed. Norris: Norris developed three yield criteria for mutually orthogonal planes. Each criterion contains quadratic stress terms (no linear terms). Nine coefficients are determined from uniaxial and pure shear tests. Tensile strengths are used when the corresponding stresses are tensile. Compressive strengths are used when the corresponding stresses are compressive. Extended YamadaSun: Three yield criteria are reported for mutually orthogonal planes. Each criterion predicts that the normal and shear stresses are mutually weakening (the presence of shear stress reduces the strength below that measured in uniaxial stress tests). Nine coefficients are determined from uniaxial and pure shear tests. Hashin: Hashin formulated a quadratic stress polynomial in terms of the invariants of a transversely isotropic material. Separate formulations are identified for parallel and perpendicular modes by assuming that failure is produced by the normal and shear stresses acting on the failure plane. In addition, the parallel and perpendicular modes are subdivided into tensile and compressive modes. Assumptions include: (1) biaxial compressive strength perpendicular to the grain is much greater than the uniaxial compressive strength and (2) shear stress does not contribute to compressive failure parallel to the grain. All coefficients are determined from six uniaxial and shear strengths. Modified Hashin (extended form of Hashin’s criteria): More terms are retained in this modified form than in the original form because fewer assumptions are made regarding material behavior. All coefficients are determined from six uniaxial and shear strengths. C.2 FORM OF CRITERIAHere, we give the functional form of the various failure criteria that were evaluated in section C.1 for modeling the strength of wood. Both orthotropic and transversely isotropic criteria are reported.
Here, X, Y, and Z are the strengths in the longitudinal, tangential, and radial directions, respectively, and S is the shear strength. The subscripts T and C refer to the tensile and compressive components, respectively. Maximum Stress: This is one of the most common limit theories. Failure occurs when any component of stress in the principal material directions exceeds its corresponding strength. Its application to wood as an orthotropic material is: Nine independent modes of failure are predicted: tensile, compressive, and shear failure parallel to the grain; tensile, compressive, and shear failure in the tangential direction; and tensile, compressive, and shear failure in the radial direction. The number of failure modes reduces to six for a transversely isotropic material. TsaiWu: Tsai and Wu developed a stress tensor component polynomial theory as a failure criterion for anisotropic materials.^{(29)} A reduced form of their criterion is applicable to transversely isotropic materials. The criterion contains both linear and quadratic stress terms. Failure occurs when the following equation is satisfied: Seven coefficients must be defined for wood modeled as a threedimensional transversely isotropic material. Six coefficients (F_{1}, F_{2}, F_{11}, F_{22}, F_{23}, and F_{66}) are determined from uniaxial and shear tests on unidirectional specimens. Each of the coefficients F_{1}, F_{2}, F_{11}, F_{22}, and F_{23} includes contributions from both tensile and compressive strengths: One coefficient, F_{12}, must be determined from biaxial tests, a variety of which are available. Different biaxial tests produce different values of F_{12}. The choice was to fit F_{12} to offaxis compression test data at 45 degrees: Here, s is the biaxial strength measured in the principal material directions. It is equal to half the ultimate strength measured in offaxis tests at 45 degrees. If s = X_{c}Y_{c} / (X_{c} + Y_{c}), then the TsaiWu model will be in agreement with Hankinson’s twodimensional formula plotted in ultimate stress versus grain angle space. The failure envelope is a smooth surface in stress space. Only the onset of failure is predicted, not the mode of failure. Hoffman: Hill generalized von Mises’ distortional energy criterion for isotropic materials to include orthotropic materials.^{(30)} Failure occurs when the following equation is satisfied: The six coefficients (A, B, D, E, F, and G) are determined from uniaxial stress and pure shear tests. However, Hill’s orthotropic criterion is not directly applicable to wood materials because it does not model different strengths in tension and compression. Hoffman modified Hill’s quadratic criterion by adding linear stress terms that take into account different strengths in tension and compression.^{(31)} Failure occurs when the following equation is satisfied: This criterion predicts a parabolic increase in strength with confining pressure. The nine coefficients are determined from uniaxial stress and pure shear tests. The criterion is readily simplified for materials with transversely isotropic strength values. One advantage of this criterion is that the interaction terms are not based on biaxial data, so it is easier to fit than the TsaiWu criterion. One disadvantage of this criterion (and the TsaiWu criterion) is that the onset of failure is predicted, but not the mode of failure. Norris: Tsai and Azzi simplified the Hill criterion to account for transverse isotropy and plane stress conditions of composite materials:^{(32)} Tsai showed that the criterion is applicable to composites with different properties in tension and compression. Tensile strengths are used when the corresponding stresses are tensile; compressive strengths are used when the corresponding stresses are compressive. Tsai also developed two additional equations for mutually orthogonal planes (similar to equation 153) for failure analysis of threedimensional materials.^{(27)} Similarly, Norris reports three yield criteria for mutually orthogonal planes. His criteria are similar to the TsaiAzzi criteria except that the interaction terms are not biased toward one particular strength. In addition, he applied his criteria to wood materials, not composites. Norris’s criterion for the 12 (LR) plane is as follows: Similar equations can be written for the 13 and 23 planes by proper interchange of subscripts. This criterion for modeling wood was evaluated by using tensile strengths when the corresponding stresses are tensile, and compressive strengths when the corresponding stresses are compressive. For each of the three equations, three combinations of tensile and compressive stresses are possible. Therefore, nine modes of failure are modeled. Extended YamadaSun: Yamada and Sun developed a plane stress criterion for composites that is a degenerative form of the TsaiAzzi and Norris criteria.(33) Failure occurs when the following equation is satisfied: This criterion predicts that the normal and shear stresses are mutually weakening (the presence of shear stress reduces the strength below that measured in uniaxial stress tests). We extended this concept to three dimensions for application to wood as either an orthotropic or transversely isotropic material: Tensile strengths are used when the corresponding stresses are tensile; compressive strengths are used when the corresponding stresses are compressive. Six independent modes of failure are predicted: tensile and compressive failure in the longitudinal direction, tensile and compressive failure in the tangential direction, and tensile and compressive failure in the radial direction. The application of shear stress contributes to failure in each of these modes and is mutually weakening. Hashin: The TsaiWu and Hoffman interactive failure criteria predict when a given set of stresses will produce failure, but they do not predict the mode of failure. Hashin developed a set of interactive failure criteria in which distinct failure modes are modeled. He applied his failure criteria to fiber composite materials. Since most fiber composites are transversely isotropic (e.g., wood), Hashin defined a general failure criterion in terms of the stress invariants of a transversely isotropic material ^{(27)}. The five stress invariants (I_{1}, I_{2}, I_{3}, I_{4}, and I_{5}) are: Hashin’s threedimensional failure criterion is a quadratic stress polynomial of the general form: The I_{5} invariant does not appear in the criterion because only linear and quadratic terms are retained in this polynomial. To identify distinct failure modes, Hashin argued that failure is produced by the normal and shear stresses acting on the failure plane. For failure parallel to the grain, the failure plane is the 23 plane, acted on by stresses s_{11}, s_{12}, and s_{13}. The perpendicular stresses (s_{22}, s_{23}, and s_{33}) do not contribute to parallel failure. The implicit assumption here is that the perpendicular stresses do not impede compression bucking; thus, an interaction mechanism is not required (the term C_{12}I_{1}I_{2} is neglected). In perpendiculartothegrain failure, failure occurs in any plane with axes parallel and perpendicular to the grain. The failure plane is acted on by stresses s_{22}, s_{33}, s_{23}, s_{12}, and s_{13}. The implicit assumption here is that the stress parallel to the grain (s_{11}) does not contribute to perpendicular failure because this stress is carried almost entirely by the fibers. By applying these assumptions to the general criterion in equation 164, Hashin developed specific yield criteria for the parallel and perpendicular modes: Parallel Mode Perpendicular Mode Failure mechanisms are different for tensile and compressive modes, so Hashin further divided each criterion into tensile and compressive modes. Tension Parallel: Hashin assumed that tensile and shear stresses are mutually weakening; therefore, both contribute to tensile failure. Data from direct pull and biaxial tests are needed to solve for both coefficients (A_{f} and B_{f}). If data from a direct pull test are the only data available, then one can solve for either A_{f} or B_{f}. The failure surface remains smooth and elliptical if one solves for B_{f} and neglects A_{f}. Failure occurs when the following equation is satisfied: This criterion is the same as our extension of the YamadaSun criterion. Compression Parallel: If compressive and shear stresses are assumed to be mutually weakening, then one can develop a compression parallel criterion similar to that for tension. However, Hashin argued that there is no physically reasonable method for including the effect of shear stress, at least for composites. Therefore, he represents parallel compressive failure in simple maximum stress form: Tension Perpendicular: Data from direct pull and biaxial tests are needed to solve for both coefficients (A_{m} and B_{m}). If data from a direct pull test are the only data available, then one can solve for either A_{m} or B_{m}. The failure surface remains smooth and elliptical if one solves for B_{m} and neglects A_{m}. Failure occurs when the following equation is satisfied: Compression Perpendicular:Hashin argued that the biaxial compressive strength (Y_{cc}) of composites is much greater than the uniaxial compressive strength (Y_{c}). Therefore, he solved for both coefficients (A_{m} and B_{m}) and retained only firstorder terms in Y_{c} /Y_{cc}. Failure occurs when the following equation is satisfied: The Modified Hashin criteria predict four independent modes of failure: tensile and compressive failure parallel to the grain, and tensile and compressive failure perpendicular to the grain. Although Hashin applied these criteria to fiber composites, these criteria were also evaluated for wood. A plane stress version is currently implemented in model 22 of LSDYNA, along with an augmentation by Chang that takes into account nonlinear shear stressstrain behavior. Modified Hashin: In addition to the composite criteria proposed by Hashin, a simple modification of the Hashin criteria was evaluated. Tension and Compression Parallel: Here, it is assumed that shear stress weakens wood in compression as well as in tension. In this case, the tensile and compressive yield criteria have the following form: Tension and Compression Perpendicular: It is not clear whether the biaxial compressive strength of wood is greater or lesser than the uniaxial compressive strength. The only available data for southern yellow pine are uniaxial stress data, so no assumptions are made regarding the relative strengths in biaxial and uniaxial compression. In this case, the tensile and compressive yield criteria have the following form: The Modified Hashin criteria predict four independent modes of failure: tensile and compressive failure parallel to the grain, and tensile and compressive failure perpendicular to the grain. Hankinson: Hankinson developed an empirical formula that is frequently applied to offaxis wood tests in two dimensions.^{(16,34)} Goodman and Bodig extended the formula to three dimensions.^{(7)} Their threedimensional formula predicts the ultimate compressive strength (s_{ult}) of wood relative to the both the grain (q) and ring angles (f). The threedimensional formula has the following form: where F_{f} varies sinusoidally with the ring angle between the relative strength in the tangential direction (F_{T} = Y/X) and the relative strength in the radial direction (F_{R} = Z/X). F_{f} has the following form: Here, K is an empirical constant that is typically 0.4 for softwoods. The last term on the right of 172 is a sinusoidal correction to the straight line interpolation between the tangential (Y) and radial (Z) strengths. This correction is illustrated in figure 45. It can be compared with the data shown later in figure 48. Comparisons of Hankinson’s threedimensional formula with Douglas fir test data were previously shown in figure 2. Hankinson’s formula predicts large reductions in strength when the load is inclined at a small angle to the grain or ring, in agreement with test data. Figure 45. Compressive strength variation of clear wood is readily modeled by a sinusoidal correction in the RT plane. Source: Krieger Publishing Company ^{(16)}. For a transversely isotropic material with no variations in strength with the ring angle (F_{T} = F_{R} = F_{f}), the threedimensional formula reduces to its twodimensional form: Although Hankinson’s formula has been shown to provide good fits to offaxis test data, it is not a generalpurpose formulation that can be applied to other types of tests. Thus, it is not suitable for use in finite element codes. However, it is reported here so that it can be compared with other criteria to help in their evaluation. 
Topics: research, safety, infrastructure, structures, materials Keywords: research, safety, infrastructure, structures, materials, wood, LSDYNA, orthotropic, material model, damage, rate effects, guardrail TRT Terms: guardrails, wood Updated: 04/12/2012
