2016
DOI: 10.1016/j.engstruct.2016.02.044
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Effects of non-uniform temperature distribution on critical member temperature of steel tubular truss

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Cited by 15 publications
(9 citation statements)
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“…For sprayed-on contour board insulation, this factor is equal to the perimeter to the sectional area ratio. For box insulation, this factor is computed from formula [29]: (11) where b is I-section width, h is section height, and As is the cross-sectional area of the profile. The results presented above indicate that as the fire develops, the temperature of the members without fire-proofing insulation becomes closer to and, over time, equal to the temperature of fire gases.…”
Section: Resultsmentioning
confidence: 99%
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“…For sprayed-on contour board insulation, this factor is equal to the perimeter to the sectional area ratio. For box insulation, this factor is computed from formula [29]: (11) where b is I-section width, h is section height, and As is the cross-sectional area of the profile. The results presented above indicate that as the fire develops, the temperature of the members without fire-proofing insulation becomes closer to and, over time, equal to the temperature of fire gases.…”
Section: Resultsmentioning
confidence: 99%
“…Problems related to the description of failure modes have been the subject of discussion in many works. Articles that deserve special attention include those in [11][12][13].…”
Section: Introductionmentioning
confidence: 99%
“…As shown in Figure 14, the hysteresis model can be calculated by Equations (3), (8), (9) and (13), and the effect of damage accumulation is considered to start from the second semi-cycle. Damage degradation is considered by introducing the evolution equation of the damage variable D. The realization process of the hysteresis criterion is: the initial stress amplitude under cyclic loading is calculated by the cyclic stress-strain curve and the initial loading curve → the damage variable D n of each semi-cycle is calculated by Equation (3) → the stress amplitude σ D(n) m and the elastic modulus E D n are calculated by Equations (8) and (9) → the hysteresis curve of the nth semi-cycle can be obtained by Equation (13) → then calculate the (n + 1)th semi-cycle, and so on.…”
Section: A Model Of Hysteretic Curve With Damage Accumulationmentioning
confidence: 99%
“…The cumulative damage variable D will be valued 1 when the specimen is destroyed, and calculate the maximum plastic strain ε p m and the cumulative plastic energy dissipation in the cyclic process, then the parameter λ can be obtained use Equation (3), so the value of λ can fitaccording to Equation (14) by the test data, and the fitting results are presented in Table 6. The parameters can be fitted according to Equations (8) and (9) by the results of low-cycle fatigue test. Equations (8) and (9) can be transformed into Equations (15) and (16), and the curves of σ D(n) m σ m −D n and E D n E 0 −D n of WB1(2) are presented in Figure 15 (an example).…”
Section: The Parameter λ Of Evolutionequation Of Damage Accumulationmentioning
confidence: 99%
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