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Comparison with Current AISC Seismic Provisions 419

412

(a) (b) 413

414

(c) (d) 415

Fig. 12. Effective stress ratio (ESR) of T-sections at column DR of (a) 1%; (b) 2%; (c) 3% and 416

(d) 4%.

417 418

7. Comparison with Current AISC Seismic Provisions 419

All specimens with b/2tf and (h/tw)eq smaller than λr have a buckling strength larger than Py under 420

all loading schemes. Even when b/2tf exceeds λr, e.g. F5W1 specimens, a peak strength of at least 421

Py is still achieved. While not shown in this paper, the computational study also supports this 422

finding. As a result, the current λr limit is considered adequate for flanges in beams and columns 423

under the monotonic and cyclic loading schemes considered in this work.

424 425

From the experimental results, it is also clear that λhd is reasonable under monotonic loading. This 426

assessment is based on the observed good post-buckling responses exhibited by monotonically 427

loaded specimens with F1 and F2 flanges. The same can be said for specimens subjected to cyclic 428

axial loading for demands under the CB protocol. The degradation in tensile strength is much 429

milder than the post-buckling degradation seen under compression, which combined, will likely 430

allow most available cross-sections to carry at least 80% of their plastic moment capacity up to 431

4% rotation. Therefore, current limits on λhd for flanges appear to provide appropriate highly 432

ductile behavior for beams under cyclic loading.

433 434

Specimen F2W1-CC, which has a b/2tf smaller than the current λhd limit, exhibits an ESR of 0.78Py

435

at a NAD corresponding to 4% column drift. Equation (1) indicates that ESR reaches 0.65 at the 436

highly ductile slenderness limit. The evidence in this paper suggests that, barring other failure 437

modes such as global instability, a W24 column with slenderness characteristics similar to those 438

considered would be able “to withstand significant plastic rotation of 0.04 rad or more” per current 439

design philosophy and still support a substantial axial load. However, the key question of whether 440

the moment or axial capacities have been degraded too much by cyclic FLB is not addressed in 441

current seismic provisions. Unlike beams, where current seismic design provisions require that the 442

moment capacity be at least 80% of the plastic capacity at 4% drift, columns have no such 443

requirement. The research in this paper points out the need for more precise performance 444

requirements for columns.

445 446

8. Conclusions 447

The effect of cyclic FLB on the capacity of structural members in special moment frames was 448

experimentally and computationally investigated in this study. Nineteen half-scale T-section 449

specimens were axially loaded to represent the flange/web subassembly in the plastic hinge region 450

of a wide flange section under combined axial and flexural loading. The specimens were selected 451

to cover a wide range of slenderness ratios and subjected to three different loading schemes. The 452

loading schemes included monotonic compression, meant to obtain the flange capacity without 453

cyclic degradation, and two cyclic axial loading histories, one that reflected the axial demands on 454

beam flanges and another for column flanges under cyclic drift loading. To further study the cyclic 455

behavior of column flanges and justify the observation from the test results, a parametric 456

computational study with different slenderness ratios was performed. The effect of slenderness 457

ratios on column compression capacity due to flange strength degradation was then evaluated.

458 459

The test results showed that most T-section specimens could reach a peak strength of Py regardless 460

of the value of b/2tf, but b/2tf substantially influenced post-buckling behavior. Under monotonic 461

loading, the current value for λhd for a flange was shown to be a boundary between large buckling 462

capacity and rapid degradation after reaching peak strength. The effect of (h/tw)eq, on the other 463

hand, was shown to be secondary and became significant only when both b/2tf and (h/tw)eq were 464

large and negatively interacted with each other.

465 466

Specimens under the CB loading protocol exhibited much more severe compressive strength 467

degradation than the monotonic protocol. Depending on a specimen’s b/2tf, the compressive 468

strength dropped to as low as 0.53 Py at deformation levels that corresponded to 4% beam rotation.

469

The tensile strength had a much milder degradation rate than the compressive strength. However, 470

the required tensile strain for recovery of tensile strength after unloading from compression 471

depended on the slenderness ratio due to the effort of stretching out the buckled shape.

472 473

The backbone curves of specimens under CC loading were much higher than those for specimens 474

under CB loading and were quite close to the responses under M loading. This result was attributed 475

to the smaller tensile plastic strain demands and led to a milder cyclic degradation rate under 476

compression. Nevertheless, the degradation at higher drift levels could be substantial and could 477

compromise the axial and flexural capacities of the columns.

478 479

The experimental and computational data was used to evaluate the current AISC seismic 480

provisions. It was shown that the current λr limit is adequate for flanges in beams and columns 481

under the monotonic and cyclic loading schemes considered in this work. It was also shown that 482

λhd is reasonable for members under monotonic loading and CB loading, which is representative 483

of the demands seen in beams. The conclusion for λhd and λmd under CC loading, representative of 484

the demands seen in columns, was not definitive because the performance expectations of the 485

AISC seismic provisions are not as explicit as they are for beams. The research outlined in this 486

paper provides useful input to refine current specifications to address this issue.

487 488

The evaluation in this paper is only valid for the specific wide flange section sizes, loading 489

protocols and range of parameters studied. Although this research points out specific drawbacks 490

in the current AISC seismic provisions, additional research is needed to broaden the results and 491

draw comprehensive conclusions that warrant specification changes.

492 493

Acknowledgements 494

This work was supported by the University of Michigan and US NSF grant number ACI-1638186.

495

Any opinions, findings, conclusions, and recommendations expressed in this paper are those of the 496

authors and do not necessarily reflect the views of the sponsor.

497 498

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