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Investigation on dynamic pulse buckl...
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Zhang, Zheng.
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Investigation on dynamic pulse buckling and damage behavior of composite laminated beams subject to axial impulse.
Record Type:
Electronic resources : Monograph/item
Title/Author:
Investigation on dynamic pulse buckling and damage behavior of composite laminated beams subject to axial impulse./
Author:
Zhang, Zheng.
Description:
209 p.
Notes:
Source: Dissertation Abstracts International, Volume: 65-02, Section: B, page: 0908.
Contained By:
Dissertation Abstracts International65-02B.
Subject:
Engineering, Civil. -
Online resource:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=NQ89103
ISBN:
0612891038
Investigation on dynamic pulse buckling and damage behavior of composite laminated beams subject to axial impulse.
Zhang, Zheng.
Investigation on dynamic pulse buckling and damage behavior of composite laminated beams subject to axial impulse.
- 209 p.
Source: Dissertation Abstracts International, Volume: 65-02, Section: B, page: 0908.
Thesis (Ph.D.)--Dalhousie University (Canada), 2004.
The dynamic behavior, including pulse buckling, damage initiation and delamination growth of slender fiber-reinforced plastic (FRP) laminated beams, having initial geometric imperfections, subjected to an axial impulse was investigated numerical
ISBN: 0612891038Subjects--Topical Terms:
783781
Engineering, Civil.
Investigation on dynamic pulse buckling and damage behavior of composite laminated beams subject to axial impulse.
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Investigation on dynamic pulse buckling and damage behavior of composite laminated beams subject to axial impulse.
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209 p.
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Source: Dissertation Abstracts International, Volume: 65-02, Section: B, page: 0908.
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Adviser: Farid Taheri.
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Thesis (Ph.D.)--Dalhousie University (Canada), 2004.
520
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The dynamic behavior, including pulse buckling, damage initiation and delamination growth of slender fiber-reinforced plastic (FRP) laminated beams, having initial geometric imperfections, subjected to an axial impulse was investigated numerical
520
$a
The dynamic equilibrium equations of slender FRP beams, having initial geometric imperfections were established based on the Timoshenko beam theory, with the consideration of several parameters such as the beam's axial and transverse inertia, tr
520
$a
Pulse buckling, as an instability form (that is, the excessive growth of lateral, or out of plane displacement) can result from a single transient pulse load with a magnitude greater than that of the static Euler buckling load. Several parameter
520
$a
The investigation of dynamic damage behavior of laminated beams was also carried out for understanding the damage initiation mechanism in the beams impacted axially by a moving mass. Hashin's failure criteria was used to predict the likelihood o
520
$a
Delamination propagation characteristics of the beam were also investigated numerically and experimentally. Carbon fiber/epoxy specimens with different initial delamination length, located along beams' length and through their thickness, were ex
520
$a
The dynamics pulse-buckling response of carbon/epoxy and E-glass/epoxy laminated composite beams with [(+/-67.5)n] s angle lay-up, subject to axial impact was investigated experimentally and numerically as well. These beams exhibited plasticity
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School code: 0328.
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http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=NQ89103
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