Technical Papers
Jul 8, 2024

Flexural Behavior of GFRP–Aluminum Space Truss Strengthened with Prestressed CFRP Tendons: Experimental and Theoretical Study

Publication: Journal of Composites for Construction
Volume 28, Issue 5

Abstract

The low elastic modulus of glass fiber–reinforced polymer (GFRP) materials used in civil engineering may lead to insufficient structural stiffness in GFRP–aluminum space truss structures, limiting their ability to meet the service limit state requirements. To enhance flexural stiffness, a prestressed carbon fiber–reinforced polymer (CFRP) tendon system was developed and demonstrated. Full-scale three-point bending tests were performed to evaluate the flexural response of GFRP space truss girders, both with and without CFRP tendons. Four prestressing schemes were investigated, revealing the effect of the tendon system in enhancing stiffness. A simplified, design-oriented theoretical model using the equivalent continuum method and the force method was developed to aid structural design calculations. The model's formulas account for variable joint stiffness and equivalent shear deformation, enabling accurate stiffness evaluations. Parametric analyses were conducted on the prestress level, the girder-to-tendon stiffness ratio, and the geometric parameters of the CFRP tendon system. The results indicated that the four prestressing schemes enhanced the flexural stiffness and reduced the internal forces, validating the effectiveness of the novel prestressed FRP space truss structure. The proposed model accurately describes the prestressing enhancement mechanism and offers theoretical support for structural design.

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Data Availability Statement

All data and models generated or used during this study are available from the corresponding author upon request.

Acknowledgments

Support from the Natural Science Foundation of Jiangsu Province (BK20231028) and the National Natural Science Foundation of China (Nos. 52308295 and 52278288) are gratefully acknowledged.

Notation

The following symbols are used in this paper:
AB
cross-sectional area of solid-web beam (mm2);
AS
cross-sectional area of strut (mm2);
AT
cross-sectional area of tendon (mm2);
B
total flexural stiffness of equivalent continuum beam (kN · mm2);
B0
flexural stiffness of the upper and lower surface layers (kN · mm2);
d
length of GFRP tube with PTTCs and BBCs (mm);
dsb
length of solid ball (mm);
dsl
length of sleeve (mm);
dsp
length of sealing plate (mm);
dPTTC
length of PTTC (mm);
EB
elastic modulus of solid-web beam (GPa);
ES
elastic modulus of strut (GPa);
ET
elastic modulus of tendon (GPa);
(EA)EQ
modified axial stiffness (GPa · mm2);
(EA)GFRP
axial stiffness of GFRP tube (GPa · mm2);
(EA)PTTC
axial stiffness of PTTC (GPa · mm2);
(EA)sb
axial stiffness of solid ball (GPa · mm2);
(EA)sl
axial stiffness of sleeve (GPa · mm2);
(EA)sp
axial stiffness of sealing plate (GPa · mm2);
EI
equivalent flexural stiffness (kN · mm2);
(EI)EQ
modified flexural stiffness (kN · mm2);
(EI)GFRP
flexural stiffness of GFRP tube (kN · mm2);
(EI)PTTC
flexural stiffness of PTTC (kN · mm2);
(EI)sb
flexural stiffness of solid ball (kN · mm2);
(EI)sl
flexural stiffness of sleeve (kN · mm2);
(EI)sp
flexural stiffness of sealing plate (kN · mm2);
e, e1, e2
eccentricity from the CFRP tendon to the centroid of beams (mm);
FB1¯T(F)
axial force of the beams under virtual force (kN);
FBP¯T(F)
axial force of the beams under concentrated load (kN);
FTD1¯T(F)
axial force of the diagonal CFRP tendon under virtual force (kN);
FTDPT(F)
axial force of the diagonal CFRP tendon under concentrated load (kN);
FTH1¯T(F)
axial force of the horizontal CFRP tendon under virtual force (kN);
FTHPT(F)
axial force of the horizontal CFRP tendon under concentrated load (kN);
FS1¯T(F)
axial force of struts under virtual force (kN);
FSP¯T(F)
axial force of struts under concentrated load (kN);
G
material shear modulus of GFRP web member (GPa);
h
height of space truss girder or equivalent continuum beam (mm);
h1, h2
vertical distances from the centroid of the upper and lower surface layers to that of equivalent continuum beam (mm);
K
shear stiffness of solid-web beam (kN · mm2);
l
length of space truss girder or equivalent continuum beam (mm);
MB1¯T(F)
section moment of the beam under virtual force (kN · mm);
MBPT(F)
section moment of the beam under concentrated load (kN · mm);
N
axial force of truss member (kN);
P
concentrated load (kN);
Q
shear force (kN);
q
uniformly distributed load;
T0
initial prestress (kN);
T1
virtual force (kN);
t
thickness of equivalent continuous beam (mm);
w
midspan deflection (mm);
y
equation of the lateral deflection curve (dimensionless);
γ
shear strain (dimensionless);
δ
shear deformation (mm);
δ11, Δ1P
relative deflection of CFRP tendon (mm);
ΔP
incremental difference (kN);
Δω
incremental difference (mm);
η
girder-to-tendon stiffness ratio (dimensionless);
μ
cross-sectional shape factor (dimensionless);
ν
Poisson’s ratio (dimensionless);
ξ
shear influence coefficient (dimensionless); and
φ
angle between web member and the plane of the lower chords (rad).

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Journal of Composites for Construction
Volume 28Issue 5October 2024

History

Received: Jan 24, 2024
Accepted: May 20, 2024
Published online: Jul 8, 2024
Published in print: Oct 1, 2024
Discussion open until: Dec 8, 2024

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Ph.D. Student, College of Field Engineering, Army Engineering Univ. of PLA, Haifuxiang 1st, Qinhuai District, Nanjing 210007, China. Email: [email protected]
Lecturer, College of Field Engineering, Army Engineering Univ. of PLA, Haifuxiang 1st, Qinhuai District, Nanjing 210007, China (corresponding author). Email: [email protected]
Professor, College of Field Engineering, Army Engineering Univ. of PLA, Haifuxiang 1st, Qinhuai District, Nanjing 210007, China. Email: [email protected]

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