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static fatigue
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Published: 01 January 1996
Fig. 1 Log-log static fatigue plot of average time to failure, t , versus applied stress. Data are for vitreous silica and are taken from Ref 3 . Source: Ref 2
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Published: 01 January 2003
Fig. 2 Static fatigue curves for various hydrogen concentrations obtained by different baking times at 150 °C (300 °F). Sharp-notch high-strength steel specimens 1590 MPa (230 ksi); normal notch strength: 2070 MPa (300 ksi). Source: Ref 4
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Published: 01 January 2003
Fig. 7 Static fatigue curves for specimens of different notch sharpness. All specimens were baked for 30 min at 150 °C (300 °F). Source: Ref 68
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Published: 01 June 2024
Fig. 19 Mode I static/fatigue boundary in T300/V390. Original magnification: 2500×. Source: Ref 51
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Published: 01 January 1996
Fig. 21 Plots of fatigue with static mechanical properties for 2014, 2024, and 7075 aluminum alloys. (a) Endurance limit vs. tensile strength. (b) Endurance limit vs. yield strength. (c) Endurance limit vs. Elongation. (d) Endurance limit vs. reduction of area. Sharp notches ( K t > 12
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Published: 01 January 1996
Fig. 9 Fatigue and static strengths normalized with respect to unidirectional tensile strengths
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Published: 01 January 2000
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Published: 01 January 2000
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Published: 01 January 2001
Fig. 2 Longitudinal or transverse tensile static and fatigue specimens. (a) Ply drop-off specimen. (b) Plain specimen. (1) Bond glass-epoxy tabs with an epoxy film adhesive. (2) Specimen thickness shall not vary more than ±0.13 mm (0.005 in.) from nominal. (3) Specimen longitudinal edges shall
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Published: 01 January 2001
Fig. 3 Static and fatigue ply drop-off test specimen. (1) Bond fiberglass-epoxy tabs with epoxy film adhesive. (2) Specimen thickness shall not vary more than ±0.13 mm (0.005 in.). (3) Specimen longitudinal edges shall be parallel to 0.13 mm (0.005 in.). (4) Top end and bottom end surfaces
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Published: 01 January 2001
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Published: 01 January 2001
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Published: 15 June 2019
Fig. 7 Plots of fatigue with static mechanical properties for 2014, 2024, and 7075 aluminum alloys. (a) Endurance limit vs. tensile strength. (b) Endurance limit vs. yield strength. (c) Endurance limit vs. elongation. (d) Endurance limit vs. reduction of area. Sharp notches ( K t > 12
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Published: 01 June 2024
Fig. 20 Fracture surfaces generated under (a) pure mode II static and (b) fatigue. Original magnification: 1500×, 30° tilt. Source: Ref 72
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Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002419
EISBN: 978-1-62708-193-1
... illustrates the phenomenon of static fatigue and concludes with a discussion on the role of surface damage in strength and fatigue behavior. borosilicate glass dynamic fatigue fatigue behavior fracture behavior lifetime prediction silicate glass slow crack growth soda-lime-silicate glass static...
Abstract
This article discusses the fracture behavior of silicate glasses, more specifically, soda-lime-silicate glass, borosilicate glass and vitreous silica. It analyzes the testing and calculation of dynamic fatigue and slow-crack-growth for lifetime prediction of glasses. The article illustrates the phenomenon of static fatigue and concludes with a discussion on the role of surface damage in strength and fatigue behavior.
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003319
EISBN: 978-1-62708-176-4
... Abstract This article describes the fatigue mechanism and behavior of environmentally induced fatigue and cyclic fatigue. It discusses three basic strength test methods, namely, static, dynamic, and cyclic, along with their analytical relations for determining the fatigue parameters...
Abstract
This article describes the fatigue mechanism and behavior of environmentally induced fatigue and cyclic fatigue. It discusses three basic strength test methods, namely, static, dynamic, and cyclic, along with their analytical relations for determining the fatigue parameters and behavior of ceramics and glasses. The article explains the double torsion and double-cantilever beam fracture mechanics methods, which employ test specimens with relatively large, induced cracks. Crack growth data are typically determined directly by the observation of the crack or by devices that monitor test specimen compliance, such as clip gages and strain gages.
Book Chapter
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002417
EISBN: 978-1-62708-193-1
... in the description of cyclic failure. In the metallurgy, polymer science, and mechanical engineering communities, the word fatigue is a well-accepted term for describing the deformation and failure of materials under cyclic loading conditions. However, in the ceramics literature, the expression static fatigue...
Abstract
This article summarizes the understanding of the mechanisms and mechanical effects of fatigue processes in highly brittle materials, with particular emphasis on ceramics. It provides a discussion on room-temperature fatigue crack growth in monolithic ceramics, transformation-toughened ceramics, and ceramic composites under cyclic compression. The cyclic damage zones ahead of tensile fatigue cracks, crack propagation under cyclic tension or tension-compression loads, and elevated-temperature fatigue crack growth in monotonic and composite ceramics, are discussed. The article presents ceramic fatigue data for fatigue crack growth testing and concludes with a discussion on life prediction for ceramics or ceramic-matrix composites.
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002407
EISBN: 978-1-62708-193-1
... subjected to static, fatigue, and damage tolerance tests. Both test articles met aircraft performance specifications. The CAST program in particular is viewed by some investigators ( Ref 4 ) as the technical foundation for aircraft structural castings. The U.S. Air Force/Boeing Air-Launched Cruise Missile...
Abstract
This article reviews the fatigue and fracture properties of aluminum alloy castings, specifically alloys A356 and A357/D357 (all-T6) and alloy A201-T7, from the perspective of both design and manufacturing considerations. In addition, it provides an overview of the roles played by microstructure, manufacturing processes, test conditions, and casting design in determining the fatigue and fracture properties of aluminum casting alloys.
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002348
EISBN: 978-1-62708-193-1
... to conditions that produce fluctuating stresses and strains at some point or points and that may culminate in cracks or complete fracture after a sufficient number of fluctuations (Note 2). Note 1—In glass technology static tests of considerable duration are called ‘static fatigue’ tests, a type of test...
Abstract
This article provides ASTM standard definitions for fatigue and describes the approaches that are used to design finite or infinite life, used in a complementary sense in fatigue design. It explains four distinct phases of fatigue: nucleation, structurally dependent crack propagation, crack propagation, and final instability. The article discusses the significant role that fatigue plays in industrial design applications.
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0005695
EISBN: 978-1-62708-180-1
... Engineering Dictionary , nor are they in an ASTM glossary. Consequently, their use has no underlying, commonly accepted definition and should be avoided if possible. Other examples of terms that may be misinterpreted include static fatigue and stress cracking. The compilers also discourage the use...
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