EXAMPLE 1.39. A composite bar made up of aluminium and steel held between two supports as shown in Fig. 1.55. The bars are stress iree at the tcmperature of 8°C. What will be the tresses in the two bars when the errc if, (a) the supports are unyielding, and (b) the иррorts сomе пеarer each other by 0.1 mm. li can be assumed that the change of temperature is uniform all along the length of the bar, E for steel= 2.1x 10 kg/cm, E for alu- minium-7.4x 10% kg/cm², x 104 per °C; aAL for aluminium=23.4 x 10³ per °C. Steel bar dia. 50 mm Aluminium bar dia. 25 mm temperatnre is to 60 cm *-30 cm- %3D Fig. 1.55 coefficient of expansion for steel a, 11.7 (4.M.I.E.) %3D %3D

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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EXAMPLE 1.39. A composite bar made up of aluminium and steel
is held between two supports as shown in Fig. 1.55. The bars are stress
free at the tcmperature of
38 C. What will be the
stresses in the
when the
21°C if, (a) the supports
are unyielding, and (b) the
supports
each other by 0.1 mm. li
can be assumed that the
change of temperature is
uniform all along the length
of the bar, E for steel=
2.1x 10 kg/cm", E for alu-
minium-7.4x 105 kg/cm2, coefficient of expansion for steel a,=11.7
two bars
temperatnre is
Steel bar
dia. 50 mm
Aluminium bar
dia. 25 mm
come пеarer
to
60 cm-
-30 cm-
Fig. 1.55
x 10
per °C; aA for aluminium=23.4 x 10' per °C.
(4.M.I.E.)
Transcribed Image Text:Scanned by CamScanner EXAMPLE 1.39. A composite bar made up of aluminium and steel is held between two supports as shown in Fig. 1.55. The bars are stress free at the tcmperature of 38 C. What will be the stresses in the when the 21°C if, (a) the supports are unyielding, and (b) the supports each other by 0.1 mm. li can be assumed that the change of temperature is uniform all along the length of the bar, E for steel= 2.1x 10 kg/cm", E for alu- minium-7.4x 105 kg/cm2, coefficient of expansion for steel a,=11.7 two bars temperatnre is Steel bar dia. 50 mm Aluminium bar dia. 25 mm come пеarer to 60 cm- -30 cm- Fig. 1.55 x 10 per °C; aA for aluminium=23.4 x 10' per °C. (4.M.I.E.)
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