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inelastic cyclic buckling

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Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003573
EISBN: 978-1-62708-180-1
.... The article summarizes the general process of distortion failure analysis. It also discusses three types of distortion failures that provide useful insights into the problems of analyzing unusual mechanisms of distortion. These include elastic distortion, ratcheting, and inelastic cyclic buckling...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006797
EISBN: 978-1-62708-295-2
... A. , Mechanical Behavior of Material, Chap. 12 , Residual Stress , Addison-Wesley , 1966 , p 420 – 434 9. Preschmann C.R. and Stephens R.I. , Inelastic Cyclic Buckling, Exp . Mech. , Vol 12 ( No. 9 ), Sept 1972 , p 426 – 428 10.1007/BF02318555 10. Bickford J.H...
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003314
EISBN: 978-1-62708-176-4
... DIN 50113, 1982 Testing of Metals—Rotating Bending Fatigue Test (a) Available in the US through Global Engineering Documents, Clayton, MO Fatigue crack initiation and early growth require cyclic inelastic deformation. For alloys and metals tested at subcreep temperatures...
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003330
EISBN: 978-1-62708-176-4
... due to stress concentrations in the specimen arising from load introduction or slight eccentricities in load-specimen alignment should be minimized and that failure caused by global specimen buckling must be suppressed. Buckling and kinking of the fibers within the composite are features regarded...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002391
EISBN: 978-1-62708-193-1
... ) L + ( 1 + E m E ox h c h m ) ( 1 − ν ) 203 Buckling of oxide α Δ T = [ ( h c ) 4 a 4 + w E ox h c ] 1 / 2 α Δ T = thermal strain in oxide h c = critical oxide rupture...
Series: ASM Handbook
Volume: 14B
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v14b.a0005168
EISBN: 978-1-62708-186-3
... 9. Perzyna P. , Ed., Localization and Fracture Phenomena in Inelastic Solids , Springer-Verlag , Wien , 1998 10.1007/978-3-7091-2528-1 10. Thomason P.F. , Ductile Fracture in Metals , Pergamon Press , 1990 11. Krausz A.S. and Krausz K. , Ed., Unified...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006544
EISBN: 978-1-62708-210-5
... and elastic buckling strength of structures. For stresses above the elastic range, the tangent modulus and the secant modulus are sometimes used as the effective moduli, especially in buckling problems. Figure 3 shows how these two properties are determined from a stress-strain curve. Above the elastic...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002443
EISBN: 978-1-62708-194-8
... at the lower end. Contact problems are nonlinear and therefore computationally expensive. Additional analysis that should be considered is for the buckling of the rod, or of its flanges, due to peak compressive load. This would typically be done as a linear eigenvalue problem for a rod with low loads and long...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0001812
EISBN: 978-1-62708-180-1
... fatigue loading. Static loading may be tension, shear, bending, or torsion—either singly or in combination. Dynamic forces may result from impact or from cyclic fatigue loading, including vibration. Pure shear failures are usually obtained only when the shear load is transmitted over a very short length...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003571
EISBN: 978-1-62708-180-1
... V is the wear volume, L is the normal load, R a is the counterface roughness, S is the ultimate tensile strength of the polymer, ε is the elongation at break, N is the cyclic fatigue life of the polymer, Δε p is the inelastic strain amplitude, and α is a material constant obtained from...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002389
EISBN: 978-1-62708-193-1
... Fig. 1 Methodology for predicting crack propagation life using time-independent fracture mechanics Fig. 2 Schematic representation of mechanistic aspects of creep-fatigue. (a) Effect of cycling on cavitation damage. (b) Effect of cavitation on cyclic crack growth. Source: Ref 11...
Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.9781627081962
EISBN: 978-1-62708-196-2
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006767
EISBN: 978-1-62708-295-2
...). One failure mode theory is the Rankine (or maximum normal stress) criterion, where the maximum principal stress is used. The other is the Tresca theory based on the maximum shear stress. The Rankine criterion holds that inelastic deformation at a point begins when the maximum normal stress reaches...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003530
EISBN: 978-1-62708-180-1
... is used. The other is the Tresca theory based on the maximum shear stress. The Rankine criterion holds that inelastic deformation at a point begins when the maximum normal stress reaches the yield strength of the material. Tresca's theory states that yield at a point begins when the maximum shear stress...
Series: ASM Handbook
Volume: 4B
Publisher: ASM International
Published: 30 September 2014
DOI: 10.31399/asm.hb.v04b.a0005950
EISBN: 978-1-62708-166-5
... and the determination of related heat transfer boundary conditions. Because the focus is on aerospace alloys, in which the effects of phase transformations are usually considered negligible in simulation of distortion and residual stresses, the section on simulation of steel quenching processes in which inelastic...
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.9781627081764
EISBN: 978-1-62708-176-4
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.9781627081955
EISBN: 978-1-62708-195-5
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.9781627081702
EISBN: 978-1-62708-170-2
Series: ASM Handbook
Volume: 22B
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.hb.v22b.9781627081979
EISBN: 978-1-62708-197-9
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.9781627082006
EISBN: 978-1-62708-200-6