FATIGUE AND FRACTURE ASSESSMENT · fatigue and fracture assessment jesse stuart highway bridge...

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FATIGUE AND FRACTURE FATIGUE AND FRACTURE ASSESSMENT ASSESSMENT JESSE STUART JESSE STUART HIGHWAY BRIDGE HIGHWAY BRIDGE HUNTINGTON DISTRICT HUNTINGTON DISTRICT

Transcript of FATIGUE AND FRACTURE ASSESSMENT · fatigue and fracture assessment jesse stuart highway bridge...

Page 1: FATIGUE AND FRACTURE ASSESSMENT · fatigue and fracture assessment jesse stuart highway bridge huntington district

FATIGUE AND FRACTUREFATIGUE AND FRACTUREASSESSMENTASSESSMENT

JESSE STUARTJESSE STUARTHIGHWAY BRIDGEHIGHWAY BRIDGE

HUNTINGTON DISTRICTHUNTINGTON DISTRICT

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John J. Jaeger, Ph.D., P.E.John J. Jaeger, Ph.D., P.E.(o) 304(o) 304--399399--52545254(c) 304(c) 304--444444--60436043

US Army Corps of EngineersUS Army Corps of [email protected]@Lrh01.usace.army.mil

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View of Jesse Stuart Highway Bridge looking northView of Jesse Stuart Highway Bridge looking north(downstream) from Kentucky side of the Ohio River.(downstream) from Kentucky side of the Ohio River.

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Longitudinal stiffener termination, Girder A’, Span 11, Unit 3Longitudinal stiffener termination, Girder A’, Span 11, Unit 3

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Crack at the Termination of the Longitudinal Web StiffenersCrack at the Termination of the Longitudinal Web Stiffeners

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CloseClose--up view of cracked longitudinal stiffener termination.up view of cracked longitudinal stiffener termination.

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Web gap cracking at inside (upstream) web faceWeb gap cracking at inside (upstream) web faceat Cross Frame 1, Span 4 of Girder A, Unit 2.at Cross Frame 1, Span 4 of Girder A, Unit 2.

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Web gap cracking at outside (downstream) web face atWeb gap cracking at outside (downstream) web face atCross Frame 2, Span 4 of Girder A, Unit 2.Cross Frame 2, Span 4 of Girder A, Unit 2.

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Web gap cracking at inside (upstream) face atWeb gap cracking at inside (upstream) face atCross Frame 2, Span 4 of Girder A, Unit 2.Cross Frame 2, Span 4 of Girder A, Unit 2.

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Web gap cracking at inside (upstream) face atWeb gap cracking at inside (upstream) face atCross Frame 2, Span 4 of Girder A, Unit 2.Cross Frame 2, Span 4 of Girder A, Unit 2.

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Web gap cracking at inside (upstream) face atWeb gap cracking at inside (upstream) face atCross Frame 3, Span 4 of Girder A, Unit 2Cross Frame 3, Span 4 of Girder A, Unit 2

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Web gap cracking at inside (upstream) face atWeb gap cracking at inside (upstream) face atCross Frame 3, Span 4 of Girder A, Unit 2.Cross Frame 3, Span 4 of Girder A, Unit 2.

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Web gap cracking at outside (downstream) web face atWeb gap cracking at outside (downstream) web face atCross Frame 3, Span 4 of Girder A, Unit 2.Cross Frame 3, Span 4 of Girder A, Unit 2.

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General Types of Fatigue CrackingGeneral Types of Fatigue Cracking

LoadLoad--InducedInducedDistortionDistortion--InducedInduced

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LoadLoad--Induced Fatigue CrackingInduced Fatigue Cracking

Nominal Stress RangeNominal Stress RangeNumber of Applied Load CyclesNumber of Applied Load CyclesConnection DetailsConnection Details

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LoadLoad--Induced FatigueInduced Fatigue(Type 3 Cracking)(Type 3 Cracking)

Longitudinal Stiffener TerminationLongitudinal Stiffener Termination–– Category E DetailCategory E Detail–– Stress Range 6.3Stress Range 6.3 ksiksi < 13.0< 13.0 ksiksi–– Termination Opposite a Transverse StiffenerTermination Opposite a Transverse Stiffener

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DistortionDistortion--induced Fatigue Crackinginduced Fatigue Cracking(Type 1 & 2 Cracking)(Type 1 & 2 Cracking)

Stress Ranges ComplexStress Ranges ComplexLocalized Stresses unintended/UnknownLocalized Stresses unintended/UnknownOutOut--ofof--Plane DistortionPlane Distortion

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View of typical cross frame in Unit 2.View of typical cross frame in Unit 2.

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DistortionDistortion--Induced FatigueInduced Fatigue

Transverse Stiffener ConnectionTransverse Stiffener Connection–– “Tight Fit (No Weld)”“Tight Fit (No Weld)”

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Typical Cracks in Center Spans*Note measurements from Periodic Inspections. Blue writing is from FY01. Black writingis from FY03. Top crack grew 5/8” and the lower crack grew 1/8” in a two year period.

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View of typical cross frame in Unit 1 (and Unit 3).View of typical cross frame in Unit 1 (and Unit 3).

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FractureFracture AssessmentAssessmentThree Charpy V-Notch impact test specimens were testedfrom each of Units 2 and 3.Unit 2 web specimens averaged energy absorption is 261 ft-lbf.Unit 3 web specimens averaged energy absorption is 38 ft-lbf(low value 29 ft-lbf)Test temperature 40F corresponding to AASHTOTemperature Zone 2AASHTO required minimum energy absorbed value is 25 ft-lbf for ASTM 588 in Temperature Zone II.LEFM used to assess Type 3 crack as “thru-thickness ininfinite wide plate”.Critical crack length is conservatively twice the existing lengthof 2.25”.

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Retrofit for Type 1 and Type 2 Cracks.Retrofit for Type 1 and Type 2 Cracks.

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Retrofit for Type 3 CrackRetrofit for Type 3 Crack

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SummarySummary

42 fatigue cracks exist as of September 200342 fatigue cracks exist as of September 2003Probable cause is loadProbable cause is load--induced and distortioninduced and distortion--induced fatigue crackinginduced fatigue crackingLimited material testing indicates adequateLimited material testing indicates adequatefracture toughness for websfracture toughness for websObserved Type 1, 2, & 3 cracking does notObserved Type 1, 2, & 3 cracking does notimpose an immediate structural threat.impose an immediate structural threat.Existing web gap cracking does not reduce loadExisting web gap cracking does not reduce load--carrying capacity of girders.carrying capacity of girders.Permitted loads will be assessed and limitedPermitted loads will be assessed and limitedwhere possible.where possible.

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Discussion!Discussion!

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