The strength-to-weight ratio of a structural material is defined as its load-carrying capacity divided by its weight. For materials in tension, use a characteristic tensile stress obtained from a stress-strain curve as a measure of strength. For instance, either the yield stress or the ultimate stress could be used, depending upon the particular application. Thus, the strength-to-weight ratio R S / W for a material in tension is defined as R s / w = σ γ in which a is the characteristic stress and 7 is the weight density. Note that the ratio has units of length. Using the ultimate stress σ U as the strength parameter, calculate the strength-to-weight ratio (in units of meters) for each of the following materials: aluminum alloy 606I-T6, Douglas fir (in bending}, nylon. structural steel ASTM-A57.2, and a titanium alloy. Obtain the material properties from Tables [-1 and 1-3 of Appendix I. When a range of values is given in a table, use the average value.
The strength-to-weight ratio of a structural material is defined as its load-carrying capacity divided by its weight. For materials in tension, use a characteristic tensile stress obtained from a stress-strain curve as a measure of strength. For instance, either the yield stress or the ultimate stress could be used, depending upon the particular application. Thus, the strength-to-weight ratio R S / W for a material in tension is defined as R s / w = σ γ in which a is the characteristic stress and 7 is the weight density. Note that the ratio has units of length. Using the ultimate stress σ U as the strength parameter, calculate the strength-to-weight ratio (in units of meters) for each of the following materials: aluminum alloy 606I-T6, Douglas fir (in bending}, nylon. structural steel ASTM-A57.2, and a titanium alloy. Obtain the material properties from Tables [-1 and 1-3 of Appendix I. When a range of values is given in a table, use the average value.
Solution Summary: The author explains the strength-to-weight ratio for each material. A is brittle and B and C are ductile.
The strength-to-weight ratio of a structural material is defined as its load-carrying capacity divided by its weight. For materials in tension, use a characteristic tensile stress obtained from a stress-strain curve as a measure of strength. For instance, either the yield stress or the ultimate stress could be used, depending upon the particular application. Thus, the strength-to-weight ratio RS/Wfor a material in tension is defined as
R
s
/
w
=
σ
γ
in which a is the characteristic stress and 7 is the weight density. Note that the ratio has units of length. Using the ultimate stress
σ
U
as the strength parameter, calculate the strength-to-weight ratio (in units of meters) for each of the following materials: aluminum alloy 606I-T6, Douglas fir (in bending}, nylon. structural steel ASTM-A57.2, and a titanium alloy. Obtain the material properties from Tables [-1 and 1-3 of Appendix I. When a range of values is given in a table, use the average value.
Three wires are connected in parallel circuit. The assembly is subjected to a tension force P = 25 kN on both sides. Considering the given wire's properties, determine the stress at every wire and the deformation of wire B.
100KN
A force of 100 KN is applied on a column as shown. The
column is made from two materials. [The top one is a
functionally graded material with a linearly varying
modulus and densities. Its length is 2 meter. The density
and elastic modulus of the top material at point A are 2700
А
kg
m3
and 72 Gpa, respectively. The density and modulus of
kg
the top material at point B are 3000 and 100 Gpa. The
m
3
В
kg
bottom material is made from steel (density =7800
and
m2
modulus=200GPA). The length of the bottom material is
1m. The cross-sections of both materials comprising the
column are cylindrical with a diameter of 0.5 m.
C
ID (oijj + bị = 0) and
considering the weight and the applied force determine:
Using equilibrium
while
The stress distribution in both members
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