Structures: Sciencedirect
Structures: Sciencedirect
                                                                                   Structures
                                                     journal homepage: www.elsevier.com/locate/structures
Charalampos Baniotopoulosc
a
  Centre for Smart Infrastructure and Construction, Department of Engineering, University of Cambridge, UK
b
  Department of Civil Engineering, Liverpool John Moores University, UK
c
  Department of Civil Engineering, University of Birmingham, UK
Keywords:                                                   The use of grout-filled double-skin tubular (GFDST) sections in civil, bridge and offshore engineering applica
Composite columns                                           tions is rapidly increasing. The design of such composite members is not directly covered by design codes,
Double skin                                                 despite recent research studies investigating their performance, proposing design equations or modifying ex
Grout-filled                                                isting codified methods. Aiming to extend the available pool of structural performance data, the current study
Finite element modelling
                                                            reports the results of an extensive numerical investigation on GFDST stub-columns. Finite element (FE) models,
                                                            are developed and validated against published test data. A parametric investigation is conducted to evaluate the
                                                            effect of key parameters, including cross-sectional slenderness, hollow ratio and the effect of concrete infill on
                                                            the capacity of GFDST members. The numerically obtained load capacities along with collated test data are
                                                            utilised to assess the applicability of design strength predictions based on European Code (EC4), the American
                                                            Concrete Institute (ACI) and the analytical models proposed by Han et al. and Yu et al. Overall, the modified Yu
                                                            et al. provided strength predictions with low scatter, whereas ACI yielded overly conservative predictions
                                                            particularly for smaller hollow ratios.
    ⁎
        Corresponding author.
        E-mail address: nt431@cam.ac.uk (N.I. Tziavos).
https://doi.org/10.1016/j.istruc.2020.07.021
Received 22 March 2020; Received in revised form 10 June 2020; Accepted 9 July 2020
Available online 07 August 2020
2352-0124/ © 2020 Institution of Structural Engineers. Published by Elsevier Ltd. All rights reserved.
N.I. Tziavos, et al.                                                                                                                 Structures 27 (2020) 1623–1636
need to minimise carbon emissions. Along with the aforementioned                      1994-1-1 (EC4) [36], American Concrete Institute (ACI) [37] and the
studies and to enhance the design practice of double-skinned composite                analytical models proposed by Han et al. [8] and Yu et al. [38].
members, researchers have conducted numerical investigations on the
influence of material and geometrical parameters to generate new data
                                                                                      2. Numerical modelling
and assess existing design methods [10,13,32–35].
    Tests on GFDST members are scarce; Li et al. [12] reported 8 tests
                                                                                          The general-purpose FE software Abaqus [39] was employed for the
on stub-columns, 4 beam-columns and 2 on GFDST beams. Although
                                                                                      numerical computations. In order to verify the accuracy of the nu
the behaviour of the grout is often treated in a similar manner to that of
                                                                                      merical simulations, the numerical model was validated against test
concrete, for GFDSTs the grouted annulus is often very small resulting
                                                                                      data reported in two experimental studies [6,12], which are briefly
in higher hollow ratio (χ) values. Hollow ratio is the ratio of the in
                                                                                      discussed in Section 2.1. Sections 2.2 and 2.3 provide a detailed de
ternal steel diameter to the internal diameter of the external steel tube
                                                                                      scription on the numerical modelling assumptions, including the type of
and is a commonly used metric in CFDSTs to provide information on the
                                                                                      analyses, the adopted boundary conditions, interaction properties and
cross-sectional geometry. Typical hollow ratios in previous experi
                                                                                      the employed material models for the steel and the infill.
mental studies range from 0.2 to 0.7, whereas in offshore construction
of GFDST, members with hollow ratios greater than 0.8 are often em
ployed. The ultimate strength of GFDST stub columns, is a function of                 2.1. Selected experimental tests
the steel yield strength (fsy), the grout material compressive strength
(fgc) and the steel cross sectional properties (diameter to thickness ratio,              The experiments on stub columns reported by Tao et al. [6] and Li
D/t).                                                                                 et al. [12] are used herein to validate the FE models. The infill material
    The present paper aims to fill this gap of limited available data on              in the tests reported in [6] is concrete with a compressive strength of
the structural performance of GFDST cross-sections across a range of                  47.4 N/mm2, whereas a grout infill with a compressive strength of 51.1
hollow ratios by generating new data on the compressive capacity of                   and 54.8 N/mm2 was used in the tests reported in [12]. A total of 7
GFDST stub columns by means of numerical modelling. Initially, the                    cross-section geometries were considered, with duplicate tests per
developed FE models are validated against experiments and subse                      formed for each configuration thereby resulting in 14 experimental
quently a parametric study is carried out, investigating the effect of                tests. The hollow ratio of the selected experimental tests ranges from
cross-sectional slenderness in small and large-diameter GFDST stub-                   0.28 to 0.84. The dimensions of each specimen and the corresponding
columns. The hollow ratios for the developed FE models range from 0.4                 material properties are reported in Table 1, where L is the length of the
to 0.9. The numerically obtained strengths are subsequently compared                  specimen and Do, to, Di, ti, the diameter and thickness of the external
with design strength predictions obtained from European Code EN                       and internal steel tube respectively. A typical GFDST cross-section is
                                                                                      shown in Fig. 1, where Aso and Asi are the cross-sectional areas of the
Table 1
Dimensions and material properties of circular double skin stub-column specimens used in the validation study.
                                 Dimensions (mm)                                            Material properties
Source Test ID Do to Di ti L fsyo (N/mm2) fsyi (N/mm2) fcu (N/mm2) Pu, test (kN)
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                                                                                      outer and the inner tube respectively, Ag the cross-sectional area of the
                                                                                      grout and Ak the area of the hollow part. The average yield strength of
                                                                                      the external (fsyo) and internal steel tubes (fsyi), as obtained from tensile
         Fig. 1. Geometric properties and notation for GFDST members.
                                                                                      coupon tests, along with the cubic compressive strength (fcu) and the
                                                                                      recorded ultimate compressive strength (Pu,test) are also reported in
                                                                                      Table 1.
                                                                               1625
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Fig. 5. Comparison of axial load-shortening curves for experimental and FE models for stub-columns.
and as shown in Section 3, this assumption did not have any implication               true   =   eng (1   +   eng )                                            (1)
on the accuracy of the FE models. Fig. 3
                                                                                                                      true
                                                                                     true    = ln(1 +     eng )
                                                                                                                      E                                        (2)
2.3. Material modelling
                                                                                         Typical cement-based grouts exhibit similar behaviour to concrete
    For the steel tubulars the von Mises yield criterion with an isotropic           in compression, although a larger scatter is to be expected in test results
hardening behaviour was used. The behaviour of the steel tubes was                   particularly for higher strength material. For this purpose, for the
defined with a multi-linear stress-strain curve employing the yield and              subsequent analyses an analytical concrete model has been employed to
ultimate stress values and corresponding strains, which were experi                 describe the behaviour of the infill material in compression. In addition,
mentally obtained and reported in [12]. Cold-formed steel tubes were                 to account for the restraint on the core from the steel tubes, a confined
used in the experiments conducted by Tao et al. [6]. The yield strength              concrete model described in Ref. [15] was selected. An exemplary
for each steel section is given in Table 1, whereas the Poisson’s ratio (ν)          stress-strain curve when using the aforementioned analytical model is
was set at 0.3. The engineering stress (σeng) and strain (εeng) values               depicted in Fig. 4 comprising three stages and is described herein. The
were converted to true stress (σtrue) and strain (εtrue) following Eqs. (1)          first part of the confined stress-strain curve (AB) is described by Eq. (1),
and (2):                                                                             which was suggested by Mander et al. [42].
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Table 2                                                                                                                               uniaxial compressive stress fb0/fc0 was taken equal to 1.16 and finally
Comparison of ultimate strength of FE models against test results.                                                                    the ratio of the second stress invariant on the tensile meridian to that on
     Source                          Test ID                       Pu,   test   (kN)         Pu,   FE   (kN)   Pu,   test/FE
                                                                                                                                      the compressive meridian at initial yield was set equal to 0.725 as per
                                                                                                                                      [45]. The tensile strength of the grout was estimated from Eq. (13) as
     Tao et al. [6]                  cc2a                          1790                      1780.19           1.005                  suggested in [46] and a stress-displacement curve was defined for the
                                     cc2b                          1791                      1780.19           1.006
                                                                                                                                      tensile response of the infill material.
                                     cc3a                          1648                      1668.61           0.987
                                     cc3b                          1650                      1668.61           0.988                  fgt = 0.3(fck ) 2/3
                                     cc4a                          1435                      1311.05           1.094
                                                                                                                                                                                                              (13)
                                     cc4b                          1358                      1311.05           1.035
                                     cc5a                          904                       854.54            1.057
                                     cc5b                          898                       854.54            1.050                  3. Validation
     Li et al. [12]                  GC1-1                         751.80                    731.10            1.028
                                     GC1-2                         698.86                    731.10            0.956
                                                                                                                                           The FE models were verified against the experimental tests reported
                                     GC2-1                         935.81                    933.60            1.002
                                     GC2-2                         928.62                    933.60            0.995                  in Refs. [6,12]. The comparison between the tests and the numerical
                                     GCL-1                         8867.92                   8622.52           1.028                  models was based on the load-displacement response, the observed
                                     GCL-2                         8735.85                   8622.52           1.013                  failure modes and the ultimate axial capacity. In Fig. 5 the experimental
     Average                                                                                                   1.017                  and the numerical load – axial displacement response is compared. The
     COV                                                                                                       0.033                  initial stiffness has been accurately simulated in all the examined cases,
                                                                                                                                      demonstrating that the elastic constants and boundary conditions were
                                                                                                                                      accurately modelled. In all the models the ultimate load is also well
              fcc (     cc/ cc )                                                                                                      captured. The ultimate load (Pu, test), is compared with the numerically-
 c    =                                       ,      c   <    cc
                   1 + ( c/        cc )                                                                                  (3)          obtained one (Pu, FE) in Table 2, showing very good agreement, with an
                                                                                                                                      average ratio of 1.017 and a COV of 0.033. Typical buckling modes in
                                 Ec
where          =                                                                                                                      filled double-skin members include outward buckling of the external
                       Ec        (fcc /       cc )                                                                       (4)          tube, inward/outward buckling of the internal tube and crushing/
and f’cc, ε’cc are the confined compressive strength and corresponding                                                                cracking of the infill medium. This is confirmed in Fig. 6, where a
strain, εc the compressive strain and Ec the Young’s modulus. In this                                                                 comparison of the experimental and numerical failure modes is made.
study the experimentally defined Young’s modulus, reported in [12] is                                                                 The observed outward buckling of the external and internal steel tubes
used in the numerical models.                                                                                                         and grout/concrete crushing is accurately captured for different
                                                                                                                                      models. As shown in Fig. 5, the post-peak behaviour which was re
fcc =      c fc    + k1frp                                                                                               (5)          corded in some of the experiments has not been very well captured by
                                                                                                                                      the numerical model, which is possibly attributed to the employed
                             frp
 cc   =   c    1 + k2                                                                                                                 analytical concrete model and the plateau it forms until it reaches the
                             c fc                                                                                        (6)          ultimate strain, as illustrated in Fig. 4 and was also suggested by Thai
                                                                                                                                      et al. [47]. It is considered that this did not have any impact on the
     For the constants k1 and k2, values of 4.1 and 20.5 as suggested in
                                                                                                                                      primary focus of this study, as the ultimate load has been captured with
Richart et al. [43] were used, whereas ε’c is the unconfined concrete
                                                                                                                                      great precision. Overall, it is demonstrated that from the validation
strain at f’c and γc a strength reduction factor to account for material
                                                                                                                                      study the numerical models provide an accurate representation of the
imperfections and Dg is the diameter of the grout core. The lateral
                                                                                                                                      real conditions and a precise prediction of the experimentally observed
confining pressure (frp), on the grout is obtained from Eq. (9) as it sa
                                                                                                                                      ultimate load and corresponding failure modes which are subsequently
tisfies the cross-sections under investigation.
                                                                                                                                      used for the analytical assessment.
                            c fc          28
 c    = 0.002 +                                      , 28           c fc         82
                             54000                                                                                       (7)          4. Parametric study
 c   = 1.85Dg 0.135, 0.85                            c       1.0                                                         (8)              Upon successful validation, the numerical models were utilised to
                                                                                                                                      conduct an extensive parametric analysis, aiming to investigate the
                                                          D                                                                           effect of key parameters on the structural response of GFDST stub-col
frp = 0.006241                     0.0000357                f , 47 < D / t                    150
                                                          t syo                                                          (9)          umns. The validated models included two cross-sections with external
   The second (BC) and third (CD) stages of the stress-strain curve are                                                               diameters equal to 140 mm and 450 mm. Using these models as a basis,
described by Eqs. (10) and (11) respectively.                                                                                         two groups were considered; one with a small (group GCS) and one
                                                                                                                                      with a large diameter (group GCL). In order to get an accurate re
      =                     cu            c                                                                                           presentation of the cross-sectional response, for the numerical models
 c        c f cc   +                              (fcc         c f cc ),        cc   <   c   cu
                            cu          cc                                                                             (10)           the length of the stub-columns was taken equal to 3 times the external
                                                                                                                                      diameter. The effect of the diameter-to-thickness ratio was examined
 c    =   c f cc   ,    c   >      cu                                                                                  (11)           and four cross-sectional slenderness values equal to 50, 60, 70 and 80
where βc accounts for any confinement after the peak load was reached                                                                 (abbreviated as Dt50, Dt60, Dt70 and Dt80) were investigated for each
and was expressed in [44] as follows:                                                                                                 of the GCS and GCL groups. For the parametric study, the external and
                                                                                                                                      internal steel tubes were set to have equal D/t ratios on all FE models
                                              2
                                    D                                      D                                                          and the hollow ratio effect is further investigated in the remaining
      = 0.0000339 +                                      0.010085            + 1.3491
 c
                                    t                                      t                                           (12)           sections.
   Subsequently, the analytical compressive stress-strain curve was
converted to true values and employed in the finite element model with                                                                4.1. Cross-sectional slenderness
the Concrete Damaged Plasticity model. In this study, following a
sensitivity analysis, a dilation angle equal to 20° was found to result in                                                                For each one of the D/t values, six hollow ratio values ranging from
good agreement with the experimental tests. For the remaining para                                                                   0.4 to 0.9 with a step of 0.1 were considered. By maintaining a constant
meters, the eccentricity was set equal to 0.1, the ratio of equibiaxial to                                                            diameter to thickness ratio for both the external and the internal steel
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Fig. 6. Failure mode comparison between experiments and FE models for tests a) GC1-2, b) GC2-1, c) GCL-1, d) cc3a and infill material crushing for GCL-1 and cc3a.
tube, the same hollow ratio value χ can be achieved by either varying                outer steel tube geometric properties are constant for the examined
the diameter and the thickness of the outer tube and keeping the inner               hollow ratios. As anticipated, a smaller hollow ratio that corresponds to
tube dimensions constant or vice versa. Both cases have been in                     a larger grout thickness increases the axial capacity the GFDST stub-
vestigated and are designated as I (followed by the χ value) or O (fol              column. This is more pronounced in Fig. 7a where the outer tube has
lowed by the χ value), depending on whether the inner or outer tube                  been modified indicating that the influence of the external steel tube is
dimensions have been modified. Adopting the same assumptions de                     higher. In most cases, the overall response does not present a sudden
scribed in Section 2, a total of 96 nonlinear analyses were carried out              loss of strength but rather a stable ductile post-peak response, which is
and the results are reported in this section.                                        similar to the behaviour reported in the experiments (see Fig. 5).
    The full load-displacement path was captured during the analysis                     In Fig. 8 and Fig. 9 the numerically obtained failure loads are nor
and typical cases for a small scale and a large scale stub column with D/            malised against the squash load (Fy), and are plotted against the hollow
t = 60 are shown in Fig. 7a and Fig. 7b respectively. Note that for the              ratio for the small (GCS group) and large diameter (GCL group) FE
cases with flat load-displacement post-elastic response, where a clear               models respectively. The squash load is defined as the sum of three
peak value was not observed, the maximum load that was recorded                      terms, which are the products of the yield strength and the cross section
during the simulation was considered to be the ultimate load. In both                of the two steel tubes and the product of the compressive strength of the
cases, the effect of the change in the hollow ratio value is evident. In             grout with the cross section of the grout. For each group two cases were
Fig. 7a the inner steel tube has been kept constant, while in Fig. 7b, the           investigated, one with a constant outer steel tube and one with a
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Fig. 7. Typical load-displacement curves from parametric models for a) varying external tube and b) varying internal tube.
                                                                                            Fig. 9. Effect of steel tube cross section on the axial compressive strength of FE
Fig. 8. Effect of steel tube cross section on the axial compressive strength of FE          models in group GCL for a) constant external tube and b) constant inner tube.
models in group GCS for a) constant external tube and b) constant inner tube.
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Fig. 10. Distribution of stresses on concrete core for varying hollow ratio and constant D/t = 80.
specimens with higher and lower grout thickness.                                        previously proposed design equations and code specifications and their
    On the contrary, once the ultimate load is reached the distribution                 applicability to GFDST stub-columns. For this purpose, the design
of stresses from the inner to the outer steel tube, is significantly higher             equations provided in EC4 [36] and in the ACI code [37] for concrete
for all models. For example as shown in Fig. 10(d), the concrete stresses               filled members are modified to be applicable for double-skin tubular
closer to the inner tube are as low as 9 N/mm2 and reach values as high                 steel members and assessed herein. In addition, the analytical models
as 61 N/mm2 once closer to the external tube, demonstrating an in                      proposed in [8] and [38] are also evaluated. The accuracy of the
crease of 52 N/mm2 towards the outer tube. Similar is the range for all                 aforementioned four different design approaches to accurately predict
four cases of Fig. 10 with an axial stress range within 48–57 N/mm2.                    the resistance of double skin cross-sections in compression at ultimate
This is owing to the larger confinement that is provided on the grout                   limit state has been assessed.
core from the external steel tube when compared to the internal tube.                        In Sections 5.1–5.4, the design equations that were used, along with
This is also in agreement with findings presented in Section 4.1.                       the modifications made are presented in detail. The presently generated
    Typical failure modes that were observed in the numerical models                    numerical data along with literature collated data are summarised and
are shown in Fig. 11. For sections with large hollow ratio values –                     compared to the design guidelines in section 5.5.
hence, small grout core thickness, the lateral restraint was less pro
nounced, leading to local instabilities at locations where higher com                  5.1. Eurocode 4 (EN 1994-1-1)
pressive steel stresses occurred, as shown in Fig. 11a. As it can be ob
served in Fig. 11b and Fig. 11c, for Dt60 and Dt70 the compressive                          EN 1994-1-1 (EC4) [36] provides general rules for the design of
stresses led to a local instability in the external steel tube, resulting in a          composite steel-concrete columns and composite structures in com
failure mode similar to “elephant foot” buckling. For larger grout                      pression. Even though the plastic resistance of concrete-filled tubes in
thicknesses (Fig. 11d), material yielding was the prominent failure                     compression is detailed in Section 6.7.3.2 [36], the design of filled
mode. Finally, it is noted that the deformed shape of the model shown                   double-skin steel members is not currently covered by Eurocodes, thus a
in Fig. 11a corresponds to high applied deformations, well beyond the                   modification to existing methods was made. EC4 provides a design
ultimate load. It is believed that despite the symmetry in terms of                     equation for concrete-filled steel tubes with reinforcement by means of
geometry, loading and boundary conditions, a non-symmetric deformed                     a resistance function. The plastic resistance in compression Npl,Rd is the
shape can occur either as the result numerical instabilities/roundoff                   summation of the resistance of the components forming the cross-sec
errors that start off as infinitesimal but propagate and accumulate                     tion under investigation. The latter has been modified for GFDSTs to
throughout the analysis thus becoming significant or due to the bi                     include the grout infill and the internal steel tube replaces the steel
furcation of the symmetric solution to non-symmetric ones. This sec                    reinforcement as per Eq. (14). Similar modifications to EC4 have been
ondary bifurcation has been observed experimentally [48] and dis                       employed by Wang et al. [27], for double-skinned sections formed by
cussed analytically [49] for circular tubes in compression and it is                    stainless and high strength steel tubes.
believed that it can occur for the type of structures studied herein, al
beit, the presence of concrete infill makes the switching from an ax                                                             t o fsyo
                                                                                        PEC4 =    a A sofsyo   + A g fc 1 +                + A sifsyi
isymmetric model to a non-axisymmetric one more difficult.                                                                    c
                                                                                                                                  Do fc                                      (14)
5. Design predictions                                                                   where fc is the compressive cylinder strength of the grout and, ηa ηc and
                                                                                        are given by Eqs. (15) and (16),
  The data generated from the parametric study alongside experi
                                                                                             = 0.25(3 + 2 ¯ )      1.0                                                       (15)
mental data collected from the literature, were employed to assess                       a
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Fig. 11. Typical failure modes from FE models for varying cross-sectional slenderness.
c = 4.9 18.5 ¯ + 17 ¯ 2 0 (16) et al. [27], for CFDST stub-columns with external stainless steel tube.
                                                                                          A seo,i = A so,i
         Npl,Rk                                                                                              Do,i /t o,i fsyo,i 210000                                  (21)
¯=
          Ncr                                                               (17)          where, the subscripts (o, i) refer to the external and internal steel tube.
where Npl,Rk is the characteristic value of the plastic resistance to
compression given by Eq. (18) and evaluated as a sum of forces of the                     5.2. American Concrete Institute (ACI)
constituent elements. For the grout core a unity coefficient has been
employed to take into consideration the confinement effects.                                  ACI [37] which is the American code for the design of concrete
                                                                                          structures provides design formula for the evaluation of the ultimate
Npl,Rk = A so fsyo + A g fc + A sifsyi                                      (18)          strength of concrete-filled circular short columns. Incorporating the
    The elastic critical buckling load (Ncr), is calculated with the elastic              contribution of the inner tube, the compressive cross-sectional strength
effective stiffness (EIeff), according to Eq. (19),                                       (PACI ) of concrete-filled tubes is modified to Eq. (22) as follows:
EIeff = Eso Iso + Esi Isi + K e Eg Ig (19) PACI = A sofsyo + 0.85A g fc + A sifsyi (22)
where Ke is a correction factor for the grout core equal to 0.6, E the
Young’s modulus and the second moment of area (I) for each of the                         5.3. Han et al. [8]
components of the cross-section. According to EC 4, for circular hollow
steel sections if the local slenderness limit as defined in (20) is ex                      Han et al. carried out a series of experiments on CFDST stub col
ceeded, local buckling ought to be accounted for,                                         umns and proposed a new design Eq. (23) for the ultimate strength of
                                                                                          CFDST cross-sections, also considering the confinement offered to the
D/t     90(235/ fsy )                                                       (20)          core from the external steel tube and the influence of the hollow ratio:
    For this reason for the subsequent EC4 calculation, the cross section                 PHan = A sco fscyo + A sifsyi                                                 (23)
of the steel tubes was modified to account for local buckling according
to Eq. (21) proposed in [50] and has been recently employed by Wang                           The first term corresponds to the compressive capacity of the
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Table 3
Comparisons of small diameter FE model with design strength predictions.
  Group          FE model ID   D/t        Do (mm)   to (mm)     Di (mm)         ti (mm)           L (mm)           χ     Pu, EC 4        Pu, ACI        Pu, Han      Pu, Yu, mod
                                                                                                                          Pu, FE         Pu, FE          Pu, FE         Pu, FE
  GCS1           I0.9-Dt50     50         140.0     2.80        120.9           2.41              420.0            0.9   1.125           1.080          1.031        1.015
                 I0.8-Dt50                                      107.5           2.15                               0.8   1.126           1.156          1.060        1.031
                 I0.7-Dt50                                      94.0            1.88                               0.7   1.110           1.206          1.067        1.027
                 I0.6-Dt50                                      80.6            1.61                               0.6   1.118           1.273          1.092        1.043
                 I0.5-Dt50                                      67.2            1.34                               0.5   1.103           1.306          1.093        1.037
                 I0.4-Dt50                                      53.7            1.07                               0.4   1.094           1.337          1.096        1.034
                 O0.9-Dt50                131.9     2.63        114.0           2.28              395.8            0.9   1.089           1.046          0.998        0.983
                 O0.8-Dt50                148.4     2.96                                          445.3            0.8   1.085           1.114          1.021        0.994
                 O0.7-Dt50                169.6     3.39                                          508.9            0.7   1.079           1.176          1.042        1.002
                 O0.6-Dt50                197.9     3.95                                          593.7            0.6   1.073           1.233          1.061        1.010
                 O0.5-Dt50                237.5     4.75                                          712.5            0.5   1.071           1.290          1.084        1.022
                 O0.4-Dt50                296.8     5.93                                          890.6            0.4   1.063           1.333          1.099        1.028
  GCS2           I0.9-Dt60     60         140.0     2.33        121.8           2.03              420.0            0.9   1.118           1.074          1.022        1.008
                 I0.8-Dt60                                      108.2           1.80                               0.8   1.096           1.132          1.034        1.008
                 I0.7-Dt60                                      94.7            1.57                               0.7   1.098           1.204          1.061        1.026
                 I0.6-Dt60                                      81.2            1.35                               0.6   1.106           1.273          1.089        1.045
                 I0.5-Dt60                                      67.6            1.12                               0.5   1.106           1.323          1.105        1.055
                 I0.4-Dt60                                      54.1            0.90                               0.4   1.110           1.370          1.122        1.066
                 O0.9-Dt60                131.0     2.18        114             1.90              393.1            0.9   1.106           1.062          1.010        0.997
                 O0.8-Dt60                147.4     2.45                                          442.2            0.8   1.113           1.150          1.050        1.024
                 O0.7-Dt60                168.4     2.80                                          505.4            0.7   1.111           1.221          1.077        1.040
                 O0.6-Dt60                196.5     3.27                                          589.6            0.6   1.078           1.248          1.071        1.025
                 O0.5-Dt60                235.8     3.93                                          707.5            0.5   1.108           1.342          1.126        1.068
                 O0.4-Dt60                294.8     4.91                                          884.4            0.4   1.096           1.379          1.137        1.070
  GCS3           I0.9-Dt70     70         140.0     2.00        122.4           1.74              420.0            0.9   1.183           1.094          1.031        1.019
                 I0.8-Dt70                                      108.8           1.55                               0.8   1.156           1.157          1.046        1.024
                 I0.7-Dt70                                      95.2            1.36                               0.7   1.145           1.220          1.067        1.036
                 I0.6-Dt70                                      81.6            1.16                               0.6   1.146           1.283          1.090        1.053
                 I0.5-Dt70                                      68.0            0.97                               0.5   1.151           1.341          1.114        1.071
                 I0.4-Dt70                                      54.4            0.77                               0.4   1.157           1.390          1.134        1.086
                 O0.9-Dt70                130.3     1.86        114             1.62              391.1            0.9   1.153           1.066          1.005        0.993
                 O0.8-Dt70                146.6     2.09                                          440.0            0.8   1.151           1.152          1.042        1.020
                 O0.7-Dt70                167.6     2.39                                          502.9            0.7   1.153           1.232          1.079        1.046
                 O0.6-Dt70                195.5     2.79                                          586.7            0.6   1.152           1.297          1.109        1.067
                 O0.5-Dt70                234.7     3.35                                          704.1            0.5   1.148           1.358          1.133        1.083
                 O0.4-Dt70                293.3     4.19                                          880.1            0.4   1.133           1.393          1.143        1.085
  GCS4           I0.9-Dt80     80         140.0     1.75        122.8           1.53              420.0            0.9   1.263           1.149          1.047        1.037
                 I0.8-Dt80                                      109.2           1.36                               0.8   1.261           1.250          1.096        1.077
                 I0.7-Dt80                                      95.5            1.19                               0.7   1.224           1.297          1.102        1.076
                 I0.6-Dt80                                      81.9            1.02                               0.6   1.181           1.317          1.092        1.061
                 I0.5-Dt80                                      68.2            0.85                               0.5   1.183           1.373          1.116        1.080
                 I0.4-Dt80                                      54.6            0.68                               0.4   1.190           1.422          1.139        1.099
                 O0.9-Dt80                129.9     1.62        114.0           1.42              389.7            0.9   1.198           1.090          0.993        0.983
                 O0.8-Dt80                146.1     1.82                                          438.4            0.8   1.184           1.174          1.030        1.011
                 O0.7-Dt80                167.0     2.08                                          501.0            0.7   1.161           1.236          1.050        1.025
                 O0.6-Dt80                194.8     2.43                                          584.6            0.6   1.164           1.309          1.088        1.053
                 O0.5-Dt80                233.8     2.92                                          701.5            0.5   1.159           1.364          1.114        1.071
                 O0.4-Dt80                292.3     3.65                                          876.9            0.4   1.161           1.420          1.143        1.093
external steel tube alongside the sandwiched grout and the second term                a=
                                                                                           A so
                                                                                                , an =
                                                                                                        A so
to the compressive capacity of the internal steel tube. The cross-sec                     Ag          A g,nom                                                               (28)
tional area A sco , is given from Eq. (24)
                                                                                      where the nominal cross-section of the sandwiched grout (Ag,nom) is:
A sco = A so + A g                                                      (24)
                                                                                                    (Do       2t o) 2
                                                                                      A g,nom =
and fscyo for circular sections is given by Eq. (25),                                                     4                                                                  (29)
where a and an are the steel ratio and the nominal steel ratio as follows: where the solid ratio, Ω is defined as per Eq. (31), Ak the hollow area as
                                                                               1632
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Table 4
Comparisons of large diameter FE model with design strength predictions.
  Group          FE model ID         D/t           Do (mm)          to (mm)            Di (mm)        ti (mm)        L (mm)      χ        Pu, EC 4   Pu, ACI        Pu, Han      Pu, Yu, mod
                                                                                                                                           Pu, FE    Pu, FE          Pu, FE         Pu, FE
  GCL1           I0.9-Dt50           50            450.0            9.00               388.8          7.77           1350.0      0.9      1.101      1.052          1.010        0.990
                 I0.8-Dt50                                                             345.6          6.91                       0.8      1.121      1.145          1.061        1.021
                 I0.7-Dt50                                                             302.4          6.04                       0.7      1.111      1.201          1.077        1.021
                 I0.6-Dt50                                                             259.2          5.18                       0.6      1.113      1.265          1.102        1.032
                 I0.5-Dt50                                                             216.0          4.32                       0.5      1.116      1.322          1.124        1.042
                 I0.4-Dt50                                                             172.8          3.45                       0.4      1.128      1.383          1.153        1.060
                 O0.9-Dt50                         462.9            9.25               400.0          8.00           1388.9      0.9      1.103      1.054          1.012        0.992
                 O0.8-Dt50                         520.8            10.41                                            1562.5      0.8      1.118      1.141          1.057        1.017
                 O0.7-Dt50                         595.2            11.90                                            1785.7      0.7      1.107      1.197          1.075        1.018
                 O0.6-Dt50                         694.4            13.88                                            2083.3      0.6      1.100      1.250          1.093        1.020
                 O0.5-Dt50                         833.3            16.66                                            2500.0      0.5      1.093      1.295          1.107        1.020
                 O0.4-Dt50                         1041.7           20.83                                            3125.0      0.4      1.079      1.325          1.111        1.012
  GCL2           I0.9-Dt60           60            450.0            7.50               391.5          6.52           1350.0      0.9      1.136      1.059          1.015        0.996
                 I0.8-Dt60                                                             348.0          5.80                       0.8      1.145      1.147          1.060        1.022
                 I0.7-Dt60                                                             304.5          5.07                       0.7      1.135      1.209          1.081        1.028
                 I0.6-Dt60                                                             261.0          4.35                       0.6      1.130      1.267          1.101        1.036
                 I0.5-Dt60                                                             217.5          3.62                       0.5      1.129      1.321          1.122        1.046
                 I0.4-Dt60                                                             174.0          2.90                       0.4      1.132      1.369          1.141        1.056
                 O0.9-Dt60                         459.77           7.66               400.0          6.66           1379.3      0.9      1.146      1.068          1.024        1.004
                 O0.8-Dt60                         517.24           8.62                                             1551.7      0.8      1.150      1.152          1.065        1.026
                 O0.7-Dt60                         591.13           9.85                                             1773.4      0.7      1.140      1.214          1.087        1.032
                 O0.6-Dt60                         689.65           11.49                                            2068.9      0.6      1.135      1.273          1.110        1.040
                 O0.5-Dt60                         827.58           13.79                                            2482.8      0.5      1.134      1.326          1.132        1.048
                 O0.4-Dt60                         1034.48          17.24                                            3103.4      0.4      1.129      1.368          1.147        1.051
  GCL3           I0.9-Dt70           70            450.0            6.42               393.4          5.62           1350.0      0.9      1.200      1.085          1.008        0.990
                 I0.8-Dt70                                                             349.7          4.99                       0.8      1.198      1.175          1.054        1.019
                 I0.7-Dt70                                                             306.0          4.37                       0.7      1.182      1.240          1.079        1.030
                 I0.6-Dt70                                                             262.2          3.74                       0.6      1.170      1.297          1.100        1.040
                 I0.5-Dt70                                                             218.5          3.12                       0.5      1.166      1.350          1.121        1.051
                 I0.4-Dt70                                                             174.8          2.49                       0.4      1.195      1.464          1.217        1.135
                 O0.9-Dt70                         457.5            6.53               400.0          5.71           1372.5      0.9      1.220      1.103          1.025        1.006
                 O0.8-Dt70                         514.7            7.35                                             1544.1      0.8      1.163      1.140          1.024        0.989
                 O0.7-Dt70                         588.2            8.40                                             1764.7      0.7      1.186      1.243          1.084        1.033
                 O0.6-Dt70                         686.2            9.80                                             2058.8      0.6      1.176      1.303          1.108        1.044
                 O0.5-Dt70                         823.5            11.76                                            2470.5      0.5      1.166      1.350          1.126        1.049
                 O0.4-Dt70                         1029.4           14.70                                            3088.2      0.4      1.154      1.385          1.138        1.050
  GCL4           I0.9-Dt80           80            450.0            5.62               394.8          4.93           1350.0      0.9      1.273      1.136          1.017        0.999
                 I0.8-Dt80                                                             351.0          4.38                       0.8      1.250      1.220          1.056        1.024
                 I0.7-Dt80                                                             307.1          3.83                       0.7      1.229      1.287          1.085        1.040
                 I0.6-Dt80                                                             263.2          3.29                       0.6      1.211      1.342          1.106        1.051
                 I0.5-Dt80                                                             219.3          2.74                       0.5      1.204      1.395          1.128        1.065
                 I0.4-Dt80                                                             175.5          2.19                       0.4      1.199      1.437          1.145        1.075
                 O0.9-Dt80                         455.8            5.69               400.0          5.00           1367.5      0.9      1.279      1.141          1.021        1.004
                 O0.8-Dt80                         512.8            1.82                                             1538.4      0.8      1.256      1.225          1.062        1.029
                 O0.7-Dt80                         586.0            2.08                                             1758.2      0.7      1.231      1.289          1.088        1.041
                 O0.6-Dt80                         683.7            2.43                                             2051.2      0.6      1.222      1.353          1.118        1.058
                 O0.5-Dt80                         820.5            10.25                                            2461.5      0.5      1.185      1.373          1.114        1.045
                 O0.4-Dt80                         1025.6           12.82                                            3076.9      0.4      1.196      1.437          1.151        1.070
  [6]        cc2a, cc2b, cc3a, cc3b, cc4a,           1.179      1.344      1.127       1.118
             cc4b,                                                                                          5.5. Assessment of design predictions
             cc5a, cc5b, cc6a, cc6b, cc7a, cc7b
  [8]        DC-1, DC-2. DCc-0, DCc-1, DCc-2         1.074      1.171      0.970       0.971                    In order to evaluate the suitability of design prediction methods, the
  [12]       GC1-1, GC1-2, GC2-1, GC2-2,             1.118      1.135      1.006       0.995
             GCL-1, GCL-2
                                                                                                            bearing capacity of the FE models is normalised against the analyti
  [20]       0-1-1-1, 0-1-1-2, 0-2-1-1, 0-2-1-2,     1.053      1.175      0.991       0.959                cally-obtained strength predictions (PEC4, PACI, PHan and PYu,mod) and is
             0-2-1-2,                                                                                       shown in a tabulated format for the small (GCS) and large diameter
             0-1-2-1, 0-1-2-2, 0-2-2-1, 0-2-2-2                                                             (GCL) groups, in Table 3 and Table 4 respectively. Collated test data
  [21]       1-1-2, 2-1-2, 1-1-1, 2-1-1, 1-2-2,      1.095      1.221      1.033       1.007
                                                                                                            from the literature [6,8,12,20,21], are also employed for assessment
             2-2-2,
             1-2-1, 2-2-1                                                                                   purposes and are shown in Table 5 in a similar format, by normalising
                                                                                                            test results against design predictions. For both groups of the FE models
             Average                                 1.113      1.230      1.041       1.025
             COV                                     0.055      0.082      0.071       0.078                and collated data it is found that the strength predictions are on the safe
                                                                                                            side with varying levels of conservatism and scatter as shown in Fig. 12,
                                                                                                            where the ultimate sustained load is normalised with the predicted
                                                                                                     1633
N.I. Tziavos, et al.                                                                                                                Structures 27 (2020) 1623–1636
Fig. 12. Comparison of FE obtained compressive strength to design strength predictions for small diameter (group GCS) and large diameter (group GCL) models with
a) EC4, b) ACI, c) Han et al. [8], d) Yu et al. [38]
capacity from each design method and presented against the examined                 results in good predictions close to unity with reduced conservatism
hollow ratios. EC4 yielded safe predictions with similar trends for both            (Fig. 12d) and a coefficient of variation of 0.029 (GCS group) and 0.025
groups, with an average of 1.136 and 1.113 for GCS and GCL groups                   (GCL group). Overall, it is shown that the modified Yu et al. strength
respectively. An increasing conservatism with increasing hollow ratio               predictions are of lower conservatism. Nevertheless, Han et al. and EC4
values is observed to be consistent for small and large-diameter models             methods can also be used for design purposes of GFDST members as the
(Fig. 12a). The conservatism for high slenderness is possibly attributed            vast majority of the models are on the safe side.
to the local buckling limit suggested in [36], which is currently not                   In Fig. 13, the ultimate capacity obtained from the collated test data
explicitly defined for double skin filled tubular members, but for hollow           or the presented FE models is normalised against the plastic resistance
steel members. In this case local buckling limit was taken equal to class           design predictions from EC4 and ACI. In this case buckling of the
3 hollow sections, which does not account for the lateral restraint from            slender cross-sections is not considered, thus allowing to examine the
the infill material.                                                                applicability of the class 3 limit for GFDST stub-columns. The current
    The design predictions from ACI were found to be the most con                  limits for local buckling are also plotted for each design method.
servative amongst the design methods. Particularly for smaller hollow                   In Fig. 13a, it is shown that strength predictions are on the safe side
ratios (0.4–0.6) a high level of conservatism is shown, whereas this                for GCS, GCL groups and also for the experimental data, hence it is
reduces for models with large hollow ratios (Fig. 12b). In addition, for            suggested that further investigations are required to define a more
all the investigated models a high scatter was observed when this                   appropriate slenderness limit for GFDST stub-columns, considering the
method was employed, which can be associated with the fact that ACI                 lateral restraint provided by the infill material. This could potentially
does not account for confinement effects. Similar findings were also                result in strength predictions with less conservatism. The ACI model,
reported for CFDST stub-columns with external stainless steel tubes in              despite the ease of use resulted in very large scatter and conservatism
Wang et al. [27]. Predictions obtained from Han et al. [8] were also                for all the investigated data (Fig. 13b). Considering local buckling im
found on the safe side with a small scatter and an average of 1.076 for             proved the results as shown in Fig. 12b, however further fine tuning of
GCS and 1.088 for GCL models (Fig. 12c). Strength predictions for                   the model is required in order to consider confinement effects for
models with hollow ratios of 0.8 and 0.9 are closer to unity and overall            varying cross-sections and strain hardening of steel tubes, to allow for
with less conservatism compared to EC4 and ACI. Yu et al. [38] model                less conservative results.
                                                                             1634
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