Page 45 - Aircraft Stuctures for Engineering Student
P. 45
30 Basic elasticity
Fig. 1.16 Experimental values of principal strain using Mohr's circle.
and
(1.57)
A typical rosette would have Q = ,O = 45" in which case the principal strains are
most conveniently found using the geometry of Mohr's circle of strain. Suppose
that the arm a of the rosette is inclined at some unknown angle 8 to the maximum
principal strain as in Fig. 1.15. Then Mohr's circle of strain is as shown in Fig.
1.16; the shear strains +yay +yb and 7, do not feature in the analysis and are therefore
ignored. From Fig. 1.16
oc= +(&,+Ec)
CN =E, -0C =;(E, -E,)
QN= CM = ~ b +E,)
-OC=E~ -$(E,
The radius of the circle is CQ and
CQ = dCN2 + QN2
Hence
which simplifies to
1 J(
E,
CQ=~ - qJ2 + (E, - Eb)2
Therefore which is given by
= OC + radius of circle
is
(1.58)