Treatise on Materials Science and Technology, Volume 1 |
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Page 106
In reality , specimens made by normal manufacturing techniques will always
have regions in which the reinforcing elements are not fully ... In such a region
the applied compressive stress produces an interlaminar shear component of t =
000 .
In reality , specimens made by normal manufacturing techniques will always
have regions in which the reinforcing elements are not fully ... In such a region
the applied compressive stress produces an interlaminar shear component of t =
000 .
Page 111
Appendix : Compressive Strength of a Laminate Consider a region of initial
element misalignment as shown in Fig . A - 1 , where the reinforcing elements
make an angle do with the compression axis . Because of this misalignment , the
...
Appendix : Compressive Strength of a Laminate Consider a region of initial
element misalignment as shown in Fig . A - 1 , where the reinforcing elements
make an angle do with the compression axis . Because of this misalignment , the
...
Page 112
When the region outlined in Fig . A - 2 begins to shear and the angle of
misalignment changes from do to $ = 0 . + 40 a certain amount of work is done by
the external compressive stress AW = ( cos do - cos 0 ) ( 4cb / V ) oV AW = 4bc do
Apo ( A ...
When the region outlined in Fig . A - 2 begins to shear and the angle of
misalignment changes from do to $ = 0 . + 40 a certain amount of work is done by
the external compressive stress AW = ( cos do - cos 0 ) ( 4cb / V ) oV AW = 4bc do
Apo ( A ...
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addition alloys analysis angle applied approach associated assumed atoms average becomes bond boundary calculated complex composite concentration consider constants contribution crystal curvature curve decrease defined dependence deposition determined developed direction discussed displacement distance distribution dynamical effect elastic electron elements energy equal equation exist experimental fibers force fracture function given gives grain grain boundaries Group growth growth path illustrated increase indicate interaction interface internal friction interstitial iron laminate lattice layer length material matrix measured mechanism metal microstructural molecules nitrogen normal nucleation observed obtained occur oxygen particles peak phase plane position possible potential present produce properties region reinforcing relaxation respectively shown in Fig shows single Snoek peak solid solution strain strength stress structure substitutional surface Table temperature tungsten unit values volume waves