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Stresses straight down down the diagonal
Principal stresses
Stresses in the upper right and lower left corners
Shear stresses
Stresses in 2D equilibrium
2 normal, 1 shear
Stresses in 3D principal equilibrium
3 normal, 3 shear
Special case stresses in equilibrium
xy = yx , zx = xz , yx = zy
Angle of rotation of principle stress
xy’ = 0
Angle of rotation of shear stress
xx’ = yy’
angle of rotation of principle compared to rotation of shear
always 45 degrees apart
e
Linearized strain, simplified solution
E
green strain, nonlinear most accurate
What material characteristics can be used to identify the framework for deterring a constitutive equation
Elastic vs nonelastic, linear vs nonlinear, homogenous vs heterogenous, Isotropic vs Anisotropic
Equations for LEHI
poisson’s ration (v) , elastic modulus (E) , shear modulus G
transverse isotropic
one direction has different mechanical properties
Orthotropic
different mechanical properties in all three axes
Displacement equation
u(x) = integral (0 to L) F/EA dx = Fx/EA or u(x=l) = FL/EA
Where do you make a cut for bending
For any changes in length, force or modulus
V
Internal shear force
M
Internal moment
Bending shear stress xy
proportional to v(x), depends on cross sectional area, depends on y but opposite for normal stress
bending normal stress
0 at the center, highest at the edges
bending shear stress
0 at the edges, highest in the center
distributed load constant load equations
qa,
distributed load decreasing load
inegral (0 to L) qa +(qb-qa/L)x