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postbuckling

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Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003385
EISBN: 978-1-62708-195-5
... stiffness effects. The article presents the study of instability associated with postbuckling behavior and hygrothermal buckling in composite sandwich panels and shell panels. composites orthotropic plates anisotropic plates unsymmetric plates transverse shear stiffness postbuckling hygrothermal...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003386
EISBN: 978-1-62708-195-5
..., correlation, and observation of failures, to be able to be classified as an out-of-plane failure of the laminate due to buckling. In a postbuckled state, this compression results in out-of-plane loads around the perimeter of the delamination. These out-of-plane loads result in the sudden propagation...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003455
EISBN: 978-1-62708-195-5
... is structurally preferable. Fig. 21 Repair of MD-80 aileron skins Fig. 22 Cosmetic repairs of minor damage to MD-80 composite control surfaces If a composite elevator is produced for the MD-80, it will have much the same multirib, postbuckled (tension-field) skin design that has given...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006486
EISBN: 978-1-62708-210-5
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.9781627082105
EISBN: 978-1-62708-210-5
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003391
EISBN: 978-1-62708-195-5
.... , Schulze E. , and Minguet P. , Structural Response of Postbuckled Skin-Stiffener Panels Containing Unreinforced Penetration Holes , Proc. 5th DoD Composite Repair Technology Workshop ( Coeur d'Alene, ID ), Nov 2000 28. Rousseau C. , Baker D. , and Hethcock D...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003380
EISBN: 978-1-62708-195-5
.... , Computation of Local Energy Release Rates Along Straight and Curved Delamination Fronts of Unidirectionally DCB and ENF Specimens , Proc. 34th AIAA-SDM Conf. , La Jolla , CA , 1993 , p 1332 – 1342 27. Whitcomb J.D. , Three Dimensional Analysis of a Postbuckled Embedded Delamination , J...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003444
EISBN: 978-1-62708-195-5
Series: ASM Handbook
Volume: 6A
Publisher: ASM International
Published: 31 October 2011
DOI: 10.31399/asm.hb.v06a.a0005592
EISBN: 978-1-62708-174-0
... the residual stress is close to the critical buckling stress, the onset of buckling is hastened, and its magnitude increases with increasing imperfection size. The critical thermal load computed by the eigenvalue analysis is illustrated in the figure by a vertical dotted line. At postbuckling residual stresses...
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