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Fatigue Crack Growth in 7075-T6 Aluminum Alloy under Single-Spike Overloads and Aircraft Spectra

In the mid-1960’s, the phenomenon of flat-to slant crack growth was studied by many in the aircraft industry. At low stress-intensity factors, a fatigue-crack surface is flat (tensile mode) and the crack-front region is under plane-strain conditions (high constraint). As the crack grows with higher stress-intensity factors, a 45-degree shear lip starts to develop at the intersection of the crack front and free surfaces. With further crack extension, a complete shear failure occurs through the thickness of the sheet or plate. This behavior is the shear mode, which is under low constraint or plane-stress conditions. In 1966, Schijve found that the transition from flat-to-slant crack growth on a 2024-T3 aluminum alloy over a wide range in stress ratios (R) occurred at a constant…

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In the mid-1960’s, the phenomenon of flat-to slant crack growth was studied by many in the aircraft industry. At low stress-intensity factors, a fatigue-crack surface is flat (tensile mode) and the crack-front region is under plane-strain conditions (high constraint). As the crack grows with higher stress-intensity factors, a 45-degree shear lip starts to develop at the intersection of the crack front and free surfaces. With further crack extension, a complete shear failure occurs through the thickness of the sheet or plate. This behavior is the shear mode, which is under low constraint or plane-stress conditions. In 1966, Schijve found that the transition from flat-to-slant crack growth on a 2024-T3 aluminum alloy over a wide range in stress ratios (R) occurred at a constant crack-growth rate. Newman and Hudson showed the same behavior on 7075-T6 and Ti-8Al-1Mo-1V alloys, validating Schijve’s observation that the crack-growth rate was the key parameter for flat-to-slant crack-growth behavior.

The material considered herein is 7075-T6 aluminum alloy sheet material. Crack growth during single-spike overload-underload behavior and simulated aircraft spectrum loading are presented. The FASTRAN crack-closure based life-prediction code was used to correlate the constant-amplitude crack-growth-rate data over a wide range in stress ratios (R) and rates from threshold to near fracture, and to calculate or predict the crack-growth behavior on the single-spike overload-underload tests. Crack-closure behavior is strongly dependent upon the level of constraint. The main objective was to see if the constraint-loss region (flat-to-slant crack growth) is the primary reason for crack-growth delays after single-spike overloads. Tests were also conducted under the Mini-TWIST (standard European) transport wing spectrum. Crack-growth analyses using crack-closure theory without constraint loss were unable to predict crack growth under spike overloads or simulated aircraft spectra. However, predicted crack length against cycles with constraint-loss behavior compared reasonably well on all tests.

Artikelnummer
VAL5-2024-001

Titel
Fatigue Crack Growth in 7075-T6 Aluminum Alloy under Single-Spike Overloads and Aircraft Spectra
Autor(en)
K. F. Walker, J. C. Newman
DOI
10.48447/VAL5-2024-001
Veranstaltung
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
Jahr der Veröffentlichung
2024
Publikationsart
Tagungsmanuskript (PDF)
Sprache
Englisch
Stichwörter
cracks,damage tolerance,plasticity,spike overloads,spectrum loading

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Accelerated vibration-fatigue characterization for 3D-printed structures: Application to fused-filament-fabricated PLA samples
Accelerated vibration-fatigue characterization for 3D-printed structures: Application to fused-filament-fabricated PLA samples
M. Česnik, J. Slavič, M. Boltežar
10.48447/VAL5-2024-028
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
Accelerated fatigue test,Random-signal excitation,Specimen design,Fused filament fabrication 
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Accelerated vibration-fatigue characterization for 3D-printed structures: Application to fused-filament-fabricated PLA samples
M. Česnik, J. Slavič, M. Boltežar
10.48447/VAL5-2024-028
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Accelerated fatigue test,Random-signal excitation,Specimen design,Fused filament fabrication
Preis 25,00 €
Nur online erhältlich
Non-stationary vibration loading - Assessing its effects on structural dynamics and vibration fatigue
Autor(en): A. Trapp, P. Wolfsteiner
10.48447/VAL5-2024-053
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
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1
Non-stationary vibration loading - Assessing its effects on structural dynamics and vibration fatigue
Non-stationary vibration loading - Assessing its effects on structural dynamics and vibration fatigue
A. Trapp, P. Wolfsteiner
10.48447/VAL5-2024-053
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
structural dynamics,non-stationarity matrix,non-stationary vibration loading,random vibration fatigue 
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Non-stationary vibration loading - Assessing its effects on structural dynamics and vibration fatigue
A. Trapp, P. Wolfsteiner
10.48447/VAL5-2024-053
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
structural dynamics,non-stationarity matrix,non-stationary vibration loading,random vibration fatigue
Preis 25,00 €
Nur online erhältlich
Modal driven load tailoring for efficient vibration fatigue assessment on non-stationary processes: A versatile approach exploiting the Fatigue Damage Spectrum
Autor(en): G. Curti, T. Dengler, M. Palmieri, A. Trapp, P. Wolfsteiner, F. Cianetti, K. Schneider
10.48447/VAL5-2024-045
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
random vibration loading,non stationary loading,mission syntesis,fatigue damage spectrum,modal decomposition 
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Modal driven load tailoring for efficient vibration fatigue assessment on non-stationary processes: A versatile approach exploiting the Fatigue Damage Spectrum
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G. Curti, T. Dengler, M. Palmieri, A. Trapp, P. Wolfsteiner, F. Cianetti, K. Schneider
10.48447/VAL5-2024-045
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
random vibration loading,non stationary loading,mission syntesis,fatigue damage spectrum,modal decomposition 
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Modal driven load tailoring for efficient vibration fatigue assessment on non-stationary processes: A versatile approach exploiting the Fatigue Damage Spectrum
G. Curti, T. Dengler, M. Palmieri, A. Trapp, P. Wolfsteiner, F. Cianetti, K. Schneider
10.48447/VAL5-2024-045
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
random vibration loading,non stationary loading,mission syntesis,fatigue damage spectrum,modal decomposition
Preis 25,00 €
Nur online erhältlich
A Comparative Analysis: Time vs. Frequency Domain Definitions of the Fatemi-Socie Criterion
Autor(en): A. Niesłony, M. Böhm, M. Sgamma, A. Chiocca, F. Bucchi, F. Frendo
10.48447/VAL5-2024-037
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
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A. Niesłony, M. Böhm, M. Sgamma, A. Chiocca, F. Bucchi, F. Frendo
10.48447/VAL5-2024-037
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
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A Comparative Analysis: Time vs. Frequency Domain Definitions of the Fatemi-Socie Criterion
A. Niesłony, M. Böhm, M. Sgamma, A. Chiocca, F. Bucchi, F. Frendo
10.48447/VAL5-2024-037
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Fatemi-Socie criterion,frequency domain,vibration fatigue,multiaxial fatigue
Preis 25,00 €
Nur online erhältlich
Application of the Local Strain Approach to estimate fatigue life of clinched joints under constant and variable amplitude loading in different loading conditions
Autor(en): B. Spak, M. Schlicht, P. Froitzheim, W. Flügge, M. Kästner
10.48447/VAL5-2024-046
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Clinching,mechanical joining,Local Strain Approach,fatigue,variable amplitude loading 
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Application of the Local Strain Approach to estimate fatigue life of clinched joints under constant and variable amplitude loading in different loading conditions
Application of the Local Strain Approach to estimate fatigue life of clinched joints under constant and variable amplitude loading in different loading conditions
B. Spak, M. Schlicht, P. Froitzheim, W. Flügge, M. Kästner
10.48447/VAL5-2024-046
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
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Application of the Local Strain Approach to estimate fatigue life of clinched joints under constant and variable amplitude loading in different loading conditions
B. Spak, M. Schlicht, P. Froitzheim, W. Flügge, M. Kästner
10.48447/VAL5-2024-046
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Clinching,mechanical joining,Local Strain Approach,fatigue,variable amplitude loading
Preis 25,00 €
Nur online erhältlich
Service strength assessment of macroscopic imperfections in cast steel alloys
Autor(en): M. Stoschka, M. Horvath, W. Mössler, F. Grün
10.48447/VAL5-2024-044
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Local fatigue assessment,Total strain energy density,Cast steel,Macroscopic shrinkage defects,Service strength 
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Service strength assessment of macroscopic imperfections in cast steel alloys
Service strength assessment of macroscopic imperfections in cast steel alloys
M. Stoschka, M. Horvath, W. Mössler, F. Grün
10.48447/VAL5-2024-044
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
Local fatigue assessment,Total strain energy density,Cast steel,Macroscopic shrinkage defects,Service strength 
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Service strength assessment of macroscopic imperfections in cast steel alloys
M. Stoschka, M. Horvath, W. Mössler, F. Grün
10.48447/VAL5-2024-044
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Local fatigue assessment,Total strain energy density,Cast steel,Macroscopic shrinkage defects,Service strength
Preis 25,00 €
Nur online erhältlich
Fatigue life estimation of notched components under multiaxial non-proportional loading with variable amplitudes.
Autor(en): J. Kraft, M. Vormwald
10.48447/VAL5-2024-035
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
multiaxial fatigue,critical plane,notches 
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Fatigue life estimation of notched components under multiaxial non-proportional loading with variable amplitudes.
Fatigue life estimation of notched components under multiaxial non-proportional loading with variable amplitudes.
J. Kraft, M. Vormwald
10.48447/VAL5-2024-035
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
multiaxial fatigue,critical plane,notches 
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Fatigue life estimation of notched components under multiaxial non-proportional loading with variable amplitudes.
J. Kraft, M. Vormwald
10.48447/VAL5-2024-035
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
multiaxial fatigue,critical plane,notches
Preis 25,00 €
Nur online erhältlich
VAL5 Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
10.48447/VAL5-2024-BB
978-3-9820591-3-6
Herausgeber: A. Esderts, S. Werdin, C. Bleicher
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Berichtsband (PDF)
Englisch
Variable Amplitude Loading, VAL, VAL5 
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VAL5 Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
VAL5 Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
10.48447/VAL5-2024-BB
978-3-9820591-3-6
A. Esderts, S. Werdin, C. Bleicher
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Berichtsband (PDF)
Englisch
Variable Amplitude Loading, VAL, VAL5 
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1
VAL5 Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
10.48447/VAL5-2024-BB
978-3-9820591-3-6
A. Esderts, S. Werdin, C. Bleicher
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Berichtsband (PDF)
Englisch
Variable Amplitude Loading, VAL, VAL5
Preis 90,00 €
Nur online erhältlich
Modification of the Findley Damage Parameter for Fatigue Assessment under multi-axial proportional and non-proportional variable Amplitude Loading
Autor(en): C. Fällgren, M. Vormwald
10.48447/VAL5-2024-021
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
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1
Modification of the Findley Damage Parameter for Fatigue Assessment under multi-axial proportional and non-proportional variable Amplitude Loading
Modification of the Findley Damage Parameter for Fatigue Assessment under multi-axial proportional and non-proportional variable Amplitude Loading
C. Fällgren, M. Vormwald
10.48447/VAL5-2024-021
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
fatigue,Findley parameter,non-proportional loading,multi-axial loading,critical plane method 
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1
Modification of the Findley Damage Parameter for Fatigue Assessment under multi-axial proportional and non-proportional variable Amplitude Loading
C. Fällgren, M. Vormwald
10.48447/VAL5-2024-021
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
fatigue,Findley parameter,non-proportional loading,multi-axial loading,critical plane method
Preis 25,00 €
Nur online erhältlich
Comparative Study of Crack Growth Retardation Models for an Integral Stiffened Panel Subjected to Overload.
Autor(en): J. D. Mattos, M. A. Arbelo
10.48447/VAL5-2024-039
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Overload Retardation Effect,Fatigue Crack-Growth,Integral Stiffened Panel,Aviation Integral Panel 
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1
Comparative Study of Crack Growth Retardation Models for an Integral Stiffened Panel Subjected to Overload.
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J. D. Mattos, M. A. Arbelo
10.48447/VAL5-2024-039
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
Overload Retardation Effect,Fatigue Crack-Growth,Integral Stiffened Panel,Aviation Integral Panel 
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1
Comparative Study of Crack Growth Retardation Models for an Integral Stiffened Panel Subjected to Overload.
J. D. Mattos, M. A. Arbelo
10.48447/VAL5-2024-039
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Overload Retardation Effect,Fatigue Crack-Growth,Integral Stiffened Panel,Aviation Integral Panel
Preis 25,00 €
Nur online erhältlich
An efficient algorithm for critical plane search in random multiaxial fatigue based on Maximum Variance Method, 3D matrices and Hadamard’s element-wise product.
Autor(en): D. Benasciutti
10.48447/VAL5-2024-006
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
random loading,critical plane,maximum variance 
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An efficient algorithm for critical plane search in random multiaxial fatigue based on Maximum Variance Method, 3D matrices and Hadamard’s element-wise product.
An efficient algorithm for critical plane search in random multiaxial fatigue based on Maximum Variance Method, 3D matrices and Hadamard’s element-wise product.
D. Benasciutti
10.48447/VAL5-2024-006
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
random loading,critical plane,maximum variance 
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An efficient algorithm for critical plane search in random multiaxial fatigue based on Maximum Variance Method, 3D matrices and Hadamard’s element-wise product.
D. Benasciutti
10.48447/VAL5-2024-006
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
random loading,critical plane,maximum variance
Preis 25,00 €
Nur online erhältlich
Experimental research on fatigue self-awareness of single-process 3d-printed structures
Autor(en): M. Palmieri, A. Staffa, J. Slavic, F. Cianetti
10.48447/VAL5-2024-050
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Additive manufacturing,Vibration fatigue,Smart structures,3D-printed strain sensors 
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Experimental research on fatigue self-awareness of single-process 3d-printed structures
Experimental research on fatigue self-awareness of single-process 3d-printed structures
M. Palmieri, A. Staffa, J. Slavic, F. Cianetti
10.48447/VAL5-2024-050
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Publikationsart: Tagungsmanuskript (PDF)
Englisch
Additive manufacturing,Vibration fatigue,Smart structures,3D-printed strain sensors 
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Experimental research on fatigue self-awareness of single-process 3d-printed structures
M. Palmieri, A. Staffa, J. Slavic, F. Cianetti
10.48447/VAL5-2024-050
VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
2024
Tagungsmanuskript (PDF)
Englisch
Additive manufacturing,Vibration fatigue,Smart structures,3D-printed strain sensors
Preis 25,00 €
Nur online erhältlich