Environmental Engineering Reference
In-Depth Information
where:
h.is.a.parameter.of.length.propagation.of.the.ultrasonic.wave;
ρ.is.the.density.of.composites.(for.iberglass.1.998.g/cm 3 );
C.is.the.velocity.of.ultrasonic.propagation(.m/sec).
By.replacing.the.stress.function.from.Equation.(6.21),.the.results.are.seen.
in.Equation.(6.23):
2
d
dx
2
σ
x Q
=
=
Q h C
ρ
11
11
x
2
d
dy
2
σ
y Q
=
=
Q
h C
ρ
2
.
.
(6.23)
22
22
y
2
2
d
dy
2
τ
xy Q
=
=
Q h C
ρ
12
12
xy
2
If.the.mechanical.deformation.is.equal.to.zero,.it.is.only.considered.under.
thermal.stresses. 11
The.equation.for.thermal.stresses.would.become:
.
σ ij =Q ij ij .T.
(6.24)
where:
α.is.the.coeficient.of.temperature.expansion;
T.is.the.temperature.gradient.
Q ij .are.the.stiffness.constants.that.can.be.determined.using.an.NDE.method.
for.velocity.propagation. 4
For.the.orthotropic.nose,.thermal.radial.stresses.are:
E
1
σ
=
-Q
α
T
=
α
T
11
11
11
11
1
-
µ µ
.
12
21
.
while.the.thermal.tangential.stresses.are:
E
. (6.25)
2
σ
=
-Q
α
T
=
α
T
.
.
22
22
22
22
1
-
µ µ
12
21
Here:
E 1 ,.E 2 .are.the.moduli.of.normal.elasticity.in.the.radial.and.tangential.directions;
 
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