Stress concentration


Aim Of Experiment:

The aim of the experiment is to locate the stress concentration areas (notches) in some structural elements. We also have to measure stress in notch areas and determine shape factors (0x01 graphic
) based on measurement results.

Experimental Stand:

A reflection polariscope is the measurement instrument used. See diagram on figure 5,the polariscope can be used in both circular and linear version.

Polarizer P0x01 graphic
, and analyzer A0x01 graphic
, are placed in clamping rings attached on bearings to polariscope housing. The analyzer is capable of rotating because it is fixed in movable ring P within clamping rings. Two quarter-wave plates, C0x01 graphic
and C0x01 graphic
, fixed in their own rings within the clamping rings, are coupled by a separate gear, which ensures that both of them can be turned simultaneously by angle of 45 degrees left or right, and rotation angle is limited by guard finger K. The polariscope Is equipped with a source of white light with a halogen light-bulb.

In the image, appearing in the circular polariscope, one can see and observe interference fringes, called isochromatic lines, whose distribution is strictly related to stress field distribution (and, at the same time, to strain distribution) in the region where the coating is bounded on the examined object. On the free edge of the object, e.g. where the so-called bottom of notch is located, the normal stress, whose direction is perpendicular to the edge line, equals zero, 0x01 graphic
= 0. Equation (20) simplifies in these conditions to the form which makes it possible to directly determine the value of normal stress 0x01 graphic
of direction tangent to the edge line(see Equation 20)

The value of normal stress 0x01 graphic
of direction tangent to the edge line:

0x01 graphic
(20)

Where C is the correction coefficient depending on the proportion between rigidity of coating material and rigidity of object material.

In the case of plane state stress, the coefficient can be expressed by formula:

C0x01 graphic

Where E0x01 graphic
=0x01 graphic
(Young's modulus of coating's material).

E0x01 graphic
=0x01 graphic
(Young's modulus of A1 alloy duralumin).

0x01 graphic
=10,7mm (thickness of the coating's material).

0x01 graphic
= 7,7mm(thickness of the Object.

0x01 graphic
= 0,32 (Poisson's ratio of A1 alloy duralumin ).

0x01 graphic
= 0,00128 (model constant).

N- The order (or number) of isochromatic line.

The linear regression of the measured data

Once we had read the order of fringes from the model, we applied linear regression model in order to determine the corrected value of the fringe order. With use of this approach, we removed the systematic error of the measurement.

The relation between N and P is assumed linear and computed with use of the linear regression method.

0x01 graphic

The coefficients 0x01 graphic
and 0x01 graphic
are computed with the use of the following equations (the result from the assumption of the linearization of the data and minimizing the RMS error).

0x01 graphic
(Part I, section5,3)

0x01 graphic

0x01 graphic

No. Of model:

1

2

3

4

5

N0x01 graphic

1

1,5

2

2,5

3

P[N]

35

50

70

89

105

0x01 graphic

1,03

1,45

2,01

2,54

2,98

N0x01 graphic
-0x01 graphic

-0,03

0,05

-0,01

-0,04

0,02

N0x01 graphic

0,98

1,39

1,95

2,48

2,93

0x01 graphic
[0x01 graphic
]

70,167

100,239

140,335

178,426

210,502

0x01 graphic
0x01 graphic
[0x01 graphic
]

540,289

771,841

1080,578

1373,877

1620,867

0x01 graphic
[0x01 graphic
]

7,1

10,1

14,1

18,0

21,2

S(0x01 graphic
)

-

0,07

0.04

0,03

0,02

a0x01 graphic

9,883

9,925

9,953

9,913

9,929

Records of measurements and elaboration of results (Table 8.1

a0= 0,054 a1= 0,028

The standard deviation of random variable 0x01 graphic
according to (42) - is S(0x01 graphic
)= 0x01 graphic
= 3,67*100x01 graphic

The error analysis

Stress 0x01 graphic
on free edge of The notch, determined from (8.2), is the realization of a random variable in indirect measurements.

The estimate of variance of variable 0x01 graphic
- according to formule (50) In section 5.2 of part I - equals

0x01 graphic

The value of S(0x01 graphic
) from formula (45) see part 1, section 5.1.2 is

0x01 graphic

The isochromatic fringe orders reading error for assumed confidence level 0x01 graphic
are:

0x01 graphic

0x01 graphic
(Part1 section5,1,2 Table3)

0x01 graphic
=0,056

The limiting error of measurement of The determined stress 0x01 graphic
is then

0x01 graphic

The error of mesurement of The shape factor 0x01 graphic
can be calculated using The formula (48c):

0x01 graphic
.

The scatter Plots based on Table (8.1)

0x08 graphic

0x08 graphic

0x08 graphic

0x08 graphic

REMARKS AND CONCLUSIONS:

When a photo elastic material is subjected to a load and illuminated with polarized light from the measurement instrumentation (called a reflection polariscope), patterns of color appear which are directly proportional to the stresses and strains within the material.

Loading beyond a order 5 fringe will risk elastic deformation or fracture of the specimen.

The transition lines seen between the red and green bands are known as "fringes." The stresses in the material increase proportionally as the number of fringes increases. Closely spaced fringes means a steeper stress gradient, and uniform color represents a uniformly stressed area. Hence, the overall stress distribution can easily be studied by observing the numerical order and spacing of the fringes.

2

0x01 graphic

0x01 graphic

0x01 graphic



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