A Brief History
A Brief History
  • Introduction
  • LmnStrs --> LM 01
  • LmnStrs --> LM 02
  • LmnStrs --> LM 03
  • CiVCyld --> CV 01
  • CiVCyld--> CV 02
  • CiVCyld--> CV 03
  • PlnStrn --> PX 01
  • FuelEff --> FU 01
  • FuelEff--> FU 02
  • More
    • Introduction
    • LmnStrs --> LM 01
    • LmnStrs --> LM 02
    • LmnStrs --> LM 03
    • CiVCyld --> CV 01
    • CiVCyld--> CV 02
    • CiVCyld--> CV 03
    • PlnStrn --> PX 01
    • FuelEff --> FU 01
    • FuelEff--> FU 02
  • Introduction
  • LmnStrs --> LM 01
  • LmnStrs --> LM 02
  • LmnStrs --> LM 03
  • CiVCyld --> CV 01
  • CiVCyld--> CV 02
  • CiVCyld--> CV 03
  • PlnStrn --> PX 01
  • FuelEff --> FU 01
  • FuelEff--> FU 02

(0/90)s Laminate of Graphite Fiber in Epoxy Matrix

A screen displaying columns of numerical data and codes.

Calculated Stresses at Exact Interfacial and Free Edge Intersection

(0/90)s with continuous tensile Interlaminar Normal Stress of +390 psi

which exponentially diminishes in magnitude and turns compressive (negative and decaying) inward from the free edge (Y=1) while the transverse normal and shearing stresses both vanish at the precise intersection of the free edge and the material interface - an indication of possible delamination

(90/0)s Laminate of Graphite Fiber in Epoxy Matrix

(90/0)s with continuous compressive Interlaminar Normal Stress of -42.677 psi

which exponentially diminishes in magnitude and turns tensile (positive and decaying) inward from the free edge (Y=1) while the transverse normal and shearing stresses both vanish at the precise intersection of the free edge and the material interface - an indication of unlikely cracking-type damage.


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