Deck 10: Stresses in Beams

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A simply supported laminated beam of length L 5 0.5 m and square cross section weighs 4.8 N. Three strips are glued together to form the beam, with the allowable shear stress in the glued joint equal to 0.3 MPa.
Considering also the weight of the beam, the maximum load P that can be applied at A simply supported laminated beam of length L 5 0.5 m and square cross section weighs 4.8 N. Three strips are glued together to form the beam, with the allowable shear stress in the glued joint equal to 0.3 MPa. Considering also the weight of the beam, the maximum load P that can be applied at   /3 from the left support Is approximately:    <div style=padding-top: 35px> /3 from the left support
Is approximately: A simply supported laminated beam of length L 5 0.5 m and square cross section weighs 4.8 N. Three strips are glued together to form the beam, with the allowable shear stress in the glued joint equal to 0.3 MPa. Considering also the weight of the beam, the maximum load P that can be applied at   /3 from the left support Is approximately:    <div style=padding-top: 35px> A simply supported laminated beam of length L 5 0.5 m and square cross section weighs 4.8 N. Three strips are glued together to form the beam, with the allowable shear stress in the glued joint equal to 0.3 MPa. Considering also the weight of the beam, the maximum load P that can be applied at   /3 from the left support Is approximately:    <div style=padding-top: 35px>
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A simply supported steel beam of length L 5 1.5 m and rectangular cross section ( A simply supported steel beam of length L 5 1.5 m and rectangular cross section (   carries a uniform load of   48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately:    <div style=padding-top: 35px> carries a uniform load of A simply supported steel beam of length L 5 1.5 m and rectangular cross section (   carries a uniform load of   48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately:    <div style=padding-top: 35px> 48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately: A simply supported steel beam of length L 5 1.5 m and rectangular cross section (   carries a uniform load of   48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately:    <div style=padding-top: 35px> A simply supported steel beam of length L 5 1.5 m and rectangular cross section (   carries a uniform load of   48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately:    <div style=padding-top: 35px>
Question
A bimetallic beam of aluminum ( A bimetallic beam of aluminum (   110 GPa) strips has a width of b 5 25 mm; each strip has a thickness of t 5 1.5 mm. A bending moment of 1.75 N ? m is applied about The z axis. The ratio of the maximum stress in aluminum to that in copper is approximately:   (A) 0.6 (B) 0.8 (C) 1.0 (D) 1.5<div style=padding-top: 35px> 110 GPa) strips has a width of b 5 25 mm; each strip has a thickness of t 5 1.5 mm. A bending moment of 1.75 N ? m is applied about
The z axis. The ratio of the maximum stress in aluminum to that in copper is approximately: A bimetallic beam of aluminum (   110 GPa) strips has a width of b 5 25 mm; each strip has a thickness of t 5 1.5 mm. A bending moment of 1.75 N ? m is applied about The z axis. The ratio of the maximum stress in aluminum to that in copper is approximately:   (A) 0.6 (B) 0.8 (C) 1.0 (D) 1.5<div style=padding-top: 35px>
(A) 0.6
(B) 0.8
(C) 1.0
(D) 1.5
Question
A cantilever wood pole carries force P 5 300 N applied at its free end, as well as its own weight (weight density 5 A cantilever wood pole carries force P 5 300 N applied at its free end, as well as its own weight (weight density 5   ). The length of the pole is L 5 0.75 m and the allowable bending stress is 14 MPa. The   required diameter of the pole is approximately:   (A) 4.2 cm (B) 5.5 cm (C) 6.1 cm (D) 8.5 cm<div style=padding-top: 35px> ). The length of the pole is L 5 0.75 m and the allowable bending stress is 14 MPa. The A cantilever wood pole carries force P 5 300 N applied at its free end, as well as its own weight (weight density 5   ). The length of the pole is L 5 0.75 m and the allowable bending stress is 14 MPa. The   required diameter of the pole is approximately:   (A) 4.2 cm (B) 5.5 cm (C) 6.1 cm (D) 8.5 cm<div style=padding-top: 35px> required diameter of the pole is approximately: A cantilever wood pole carries force P 5 300 N applied at its free end, as well as its own weight (weight density 5   ). The length of the pole is L 5 0.75 m and the allowable bending stress is 14 MPa. The   required diameter of the pole is approximately:   (A) 4.2 cm (B) 5.5 cm (C) 6.1 cm (D) 8.5 cm<div style=padding-top: 35px>
(A) 4.2 cm
(B) 5.5 cm
(C) 6.1 cm
(D) 8.5 cm
Question
A simply supported wood beam (L 5 5 m) with rectangular cross section (b 5 200 mm, h 5 280 mm) car- ries uniform load q 5 6.5 kN/m includes the weight of the beam. The maximum flexural stress is approximately: A simply supported wood beam (L 5 5 m) with rectangular cross section (b 5 200 mm, h 5 280 mm) car- ries uniform load q 5 6.5 kN/m includes the weight of the beam. The maximum flexural stress is approximately:   (A) 8.7 MPa (B) 10.1 MPa (C) 11.4 MPa (D) 14.3 MPa<div style=padding-top: 35px>
(A) 8.7 MPa
(B) 10.1 MPa
(C) 11.4 MPa
(D) 14.3 MPa
Question
A steel hanger with solid cross section has horizontal force P 5 5.5 kN applied at free end D. Dimension variable b 5 175 mm and allowable normal stress is 150 MPa. Neglect self-weight of the hanger. The required
Diameter of the hanger is approximately: A steel hanger with solid cross section has horizontal force P 5 5.5 kN applied at free end D. Dimension variable b 5 175 mm and allowable normal stress is 150 MPa. Neglect self-weight of the hanger. The required Diameter of the hanger is approximately:   (A) 5 cm (B) 7 cm (C) 10 cm (D) 13 cm<div style=padding-top: 35px>
(A) 5 cm
(B) 7 cm
(C) 10 cm
(D) 13 cm
Question
A rectangular beam with semicircular notches has dimen sions A rectangular beam with semicircular notches has dimen sions   maximum allowable bending stress in the plastic beam is   (A) 12 mm (B) 20 mm (C) 28 mm (D) 32 mm  <div style=padding-top: 35px> maximum allowable bending stress in the plastic beam is A rectangular beam with semicircular notches has dimen sions   maximum allowable bending stress in the plastic beam is   (A) 12 mm (B) 20 mm (C) 28 mm (D) 32 mm  <div style=padding-top: 35px> (A) 12 mm (B) 20 mm
(C) 28 mm
(D) 32 mm
A rectangular beam with semicircular notches has dimen sions   maximum allowable bending stress in the plastic beam is   (A) 12 mm (B) 20 mm (C) 28 mm (D) 32 mm  <div style=padding-top: 35px>
Question
A cast iron pipe ( A cast iron pipe (   75 mm) is lifted by a hoist. The lift points are 6 m apart. The maximum bending stress in the pipe is approximately:    <div style=padding-top: 35px> 75 mm) is lifted by a hoist. The lift points are 6 m apart. The maximum bending stress in the pipe is approximately: A cast iron pipe (   75 mm) is lifted by a hoist. The lift points are 6 m apart. The maximum bending stress in the pipe is approximately:    <div style=padding-top: 35px> A cast iron pipe (   75 mm) is lifted by a hoist. The lift points are 6 m apart. The maximum bending stress in the pipe is approximately:    <div style=padding-top: 35px>
Question
Two thin cables, each having a diameter of d 5 t/6 and carrying tensile loads P, are bolted to the top of a rectangular steel block with cross-sectional dimensions Two thin cables, each having a diameter of d 5 t/6 and carrying tensile loads P, are bolted to the top of a rectangular steel block with cross-sectional dimensions   . The ratio of the maximum tensile to compressive Stress in the block due to loads P is:    <div style=padding-top: 35px> . The ratio of the maximum tensile to compressive
Stress in the block due to loads P is: Two thin cables, each having a diameter of d 5 t/6 and carrying tensile loads P, are bolted to the top of a rectangular steel block with cross-sectional dimensions   . The ratio of the maximum tensile to compressive Stress in the block due to loads P is:    <div style=padding-top: 35px> Two thin cables, each having a diameter of d 5 t/6 and carrying tensile loads P, are bolted to the top of a rectangular steel block with cross-sectional dimensions   . The ratio of the maximum tensile to compressive Stress in the block due to loads P is:    <div style=padding-top: 35px>
Question
An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    <div style=padding-top: 35px> . The beam cross section has a width of 50 mm and a height of 170 mm.
Allowable bending stress is 95 MPa and allowable shear stress An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    <div style=padding-top: 35px> The permissible value of load inten-
Sity An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    <div style=padding-top: 35px> is approximately: An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    <div style=padding-top: 35px> An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    <div style=padding-top: 35px>
Question
      (A) 0.5 (B) 0.7 (C) 1.2 (D) 1.5<div style=padding-top: 35px>       (A) 0.5 (B) 0.7 (C) 1.2 (D) 1.5<div style=padding-top: 35px>       (A) 0.5 (B) 0.7 (C) 1.2 (D) 1.5<div style=padding-top: 35px>
(A) 0.5
(B) 0.7
(C) 1.2
(D) 1.5
Question
    68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses<div style=padding-top: 35px>     68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses<div style=padding-top: 35px> 68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:     68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses<div style=padding-top: 35px>     68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses<div style=padding-top: 35px>     68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses<div style=padding-top: 35px> Plane stress and strain; principal stresses
Question
A beam with an overhang is loaded by a uniform load of 3 kN/m over its entire length. Moment of iner- tia A beam with an overhang is loaded by a uniform load of 3 kN/m over its entire length. Moment of iner- tia   and distances to top and bottom of the beam cross section are 20 mm and 66.4 mm, Respectively. It is known that reactions at A and B are 4.5 kN and 13.5 kN, respectively. The maximum bending Stress in the beam is approximately:    <div style=padding-top: 35px> and distances to top and bottom of the beam cross section are 20 mm and 66.4 mm,
Respectively. It is known that reactions at A and B are 4.5 kN and 13.5 kN, respectively. The maximum bending
Stress in the beam is approximately: A beam with an overhang is loaded by a uniform load of 3 kN/m over its entire length. Moment of iner- tia   and distances to top and bottom of the beam cross section are 20 mm and 66.4 mm, Respectively. It is known that reactions at A and B are 4.5 kN and 13.5 kN, respectively. The maximum bending Stress in the beam is approximately:    <div style=padding-top: 35px> A beam with an overhang is loaded by a uniform load of 3 kN/m over its entire length. Moment of iner- tia   and distances to top and bottom of the beam cross section are 20 mm and 66.4 mm, Respectively. It is known that reactions at A and B are 4.5 kN and 13.5 kN, respectively. The maximum bending Stress in the beam is approximately:    <div style=padding-top: 35px>
Question
An aluminum light pole weighs 4300 N and supports an arm of weight 700 N, with the arm center of gravity at 1.2 m left of the centroidal axis of the pole. A wind force of 1500 N acts to the right at 7.5 m above
The base. The pole cross section at the base has an outside diameter of 235 mm and thickness of 20 mm. The
Maximum compressive stress at the base is approximately: An aluminum light pole weighs 4300 N and supports an arm of weight 700 N, with the arm center of gravity at 1.2 m left of the centroidal axis of the pole. A wind force of 1500 N acts to the right at 7.5 m above The base. The pole cross section at the base has an outside diameter of 235 mm and thickness of 20 mm. The Maximum compressive stress at the base is approximately:    <div style=padding-top: 35px> An aluminum light pole weighs 4300 N and supports an arm of weight 700 N, with the arm center of gravity at 1.2 m left of the centroidal axis of the pole. A wind force of 1500 N acts to the right at 7.5 m above The base. The pole cross section at the base has an outside diameter of 235 mm and thickness of 20 mm. The Maximum compressive stress at the base is approximately:    <div style=padding-top: 35px>
Question
A copper wire (d 5 1.5 mm) is bent around a tube of radius R 5 0.6 m. The maximum normal strain in the wire is approximately: A copper wire (d 5 1.5 mm) is bent around a tube of radius R 5 0.6 m. The maximum normal strain in the wire is approximately:    <div style=padding-top: 35px> A copper wire (d 5 1.5 mm) is bent around a tube of radius R 5 0.6 m. The maximum normal strain in the wire is approximately:    <div style=padding-top: 35px>
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Deck 10: Stresses in Beams
1
A simply supported laminated beam of length L 5 0.5 m and square cross section weighs 4.8 N. Three strips are glued together to form the beam, with the allowable shear stress in the glued joint equal to 0.3 MPa.
Considering also the weight of the beam, the maximum load P that can be applied at A simply supported laminated beam of length L 5 0.5 m and square cross section weighs 4.8 N. Three strips are glued together to form the beam, with the allowable shear stress in the glued joint equal to 0.3 MPa. Considering also the weight of the beam, the maximum load P that can be applied at   /3 from the left support Is approximately:    /3 from the left support
Is approximately: A simply supported laminated beam of length L 5 0.5 m and square cross section weighs 4.8 N. Three strips are glued together to form the beam, with the allowable shear stress in the glued joint equal to 0.3 MPa. Considering also the weight of the beam, the maximum load P that can be applied at   /3 from the left support Is approximately:    A simply supported laminated beam of length L 5 0.5 m and square cross section weighs 4.8 N. Three strips are glued together to form the beam, with the allowable shear stress in the glued joint equal to 0.3 MPa. Considering also the weight of the beam, the maximum load P that can be applied at   /3 from the left support Is approximately:
C
2
A simply supported steel beam of length L 5 1.5 m and rectangular cross section ( A simply supported steel beam of length L 5 1.5 m and rectangular cross section (   carries a uniform load of   48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately:    carries a uniform load of A simply supported steel beam of length L 5 1.5 m and rectangular cross section (   carries a uniform load of   48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately:    48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately: A simply supported steel beam of length L 5 1.5 m and rectangular cross section (   carries a uniform load of   48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately:    A simply supported steel beam of length L 5 1.5 m and rectangular cross section (   carries a uniform load of   48 kN/m that includes its own weight. The maximum transverse shear stress on the cross section at 0.25 m from the left support is approximately:
B
3
A bimetallic beam of aluminum ( A bimetallic beam of aluminum (   110 GPa) strips has a width of b 5 25 mm; each strip has a thickness of t 5 1.5 mm. A bending moment of 1.75 N ? m is applied about The z axis. The ratio of the maximum stress in aluminum to that in copper is approximately:   (A) 0.6 (B) 0.8 (C) 1.0 (D) 1.5 110 GPa) strips has a width of b 5 25 mm; each strip has a thickness of t 5 1.5 mm. A bending moment of 1.75 N ? m is applied about
The z axis. The ratio of the maximum stress in aluminum to that in copper is approximately: A bimetallic beam of aluminum (   110 GPa) strips has a width of b 5 25 mm; each strip has a thickness of t 5 1.5 mm. A bending moment of 1.75 N ? m is applied about The z axis. The ratio of the maximum stress in aluminum to that in copper is approximately:   (A) 0.6 (B) 0.8 (C) 1.0 (D) 1.5
(A) 0.6
(B) 0.8
(C) 1.0
(D) 1.5
B
4
A cantilever wood pole carries force P 5 300 N applied at its free end, as well as its own weight (weight density 5 A cantilever wood pole carries force P 5 300 N applied at its free end, as well as its own weight (weight density 5   ). The length of the pole is L 5 0.75 m and the allowable bending stress is 14 MPa. The   required diameter of the pole is approximately:   (A) 4.2 cm (B) 5.5 cm (C) 6.1 cm (D) 8.5 cm ). The length of the pole is L 5 0.75 m and the allowable bending stress is 14 MPa. The A cantilever wood pole carries force P 5 300 N applied at its free end, as well as its own weight (weight density 5   ). The length of the pole is L 5 0.75 m and the allowable bending stress is 14 MPa. The   required diameter of the pole is approximately:   (A) 4.2 cm (B) 5.5 cm (C) 6.1 cm (D) 8.5 cm required diameter of the pole is approximately: A cantilever wood pole carries force P 5 300 N applied at its free end, as well as its own weight (weight density 5   ). The length of the pole is L 5 0.75 m and the allowable bending stress is 14 MPa. The   required diameter of the pole is approximately:   (A) 4.2 cm (B) 5.5 cm (C) 6.1 cm (D) 8.5 cm
(A) 4.2 cm
(B) 5.5 cm
(C) 6.1 cm
(D) 8.5 cm
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5
A simply supported wood beam (L 5 5 m) with rectangular cross section (b 5 200 mm, h 5 280 mm) car- ries uniform load q 5 6.5 kN/m includes the weight of the beam. The maximum flexural stress is approximately: A simply supported wood beam (L 5 5 m) with rectangular cross section (b 5 200 mm, h 5 280 mm) car- ries uniform load q 5 6.5 kN/m includes the weight of the beam. The maximum flexural stress is approximately:   (A) 8.7 MPa (B) 10.1 MPa (C) 11.4 MPa (D) 14.3 MPa
(A) 8.7 MPa
(B) 10.1 MPa
(C) 11.4 MPa
(D) 14.3 MPa
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6
A steel hanger with solid cross section has horizontal force P 5 5.5 kN applied at free end D. Dimension variable b 5 175 mm and allowable normal stress is 150 MPa. Neglect self-weight of the hanger. The required
Diameter of the hanger is approximately: A steel hanger with solid cross section has horizontal force P 5 5.5 kN applied at free end D. Dimension variable b 5 175 mm and allowable normal stress is 150 MPa. Neglect self-weight of the hanger. The required Diameter of the hanger is approximately:   (A) 5 cm (B) 7 cm (C) 10 cm (D) 13 cm
(A) 5 cm
(B) 7 cm
(C) 10 cm
(D) 13 cm
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7
A rectangular beam with semicircular notches has dimen sions A rectangular beam with semicircular notches has dimen sions   maximum allowable bending stress in the plastic beam is   (A) 12 mm (B) 20 mm (C) 28 mm (D) 32 mm  maximum allowable bending stress in the plastic beam is A rectangular beam with semicircular notches has dimen sions   maximum allowable bending stress in the plastic beam is   (A) 12 mm (B) 20 mm (C) 28 mm (D) 32 mm  (A) 12 mm (B) 20 mm
(C) 28 mm
(D) 32 mm
A rectangular beam with semicircular notches has dimen sions   maximum allowable bending stress in the plastic beam is   (A) 12 mm (B) 20 mm (C) 28 mm (D) 32 mm
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8
A cast iron pipe ( A cast iron pipe (   75 mm) is lifted by a hoist. The lift points are 6 m apart. The maximum bending stress in the pipe is approximately:    75 mm) is lifted by a hoist. The lift points are 6 m apart. The maximum bending stress in the pipe is approximately: A cast iron pipe (   75 mm) is lifted by a hoist. The lift points are 6 m apart. The maximum bending stress in the pipe is approximately:    A cast iron pipe (   75 mm) is lifted by a hoist. The lift points are 6 m apart. The maximum bending stress in the pipe is approximately:
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9
Two thin cables, each having a diameter of d 5 t/6 and carrying tensile loads P, are bolted to the top of a rectangular steel block with cross-sectional dimensions Two thin cables, each having a diameter of d 5 t/6 and carrying tensile loads P, are bolted to the top of a rectangular steel block with cross-sectional dimensions   . The ratio of the maximum tensile to compressive Stress in the block due to loads P is:    . The ratio of the maximum tensile to compressive
Stress in the block due to loads P is: Two thin cables, each having a diameter of d 5 t/6 and carrying tensile loads P, are bolted to the top of a rectangular steel block with cross-sectional dimensions   . The ratio of the maximum tensile to compressive Stress in the block due to loads P is:    Two thin cables, each having a diameter of d 5 t/6 and carrying tensile loads P, are bolted to the top of a rectangular steel block with cross-sectional dimensions   . The ratio of the maximum tensile to compressive Stress in the block due to loads P is:
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10
An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    . The beam cross section has a width of 50 mm and a height of 170 mm.
Allowable bending stress is 95 MPa and allowable shear stress An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    The permissible value of load inten-
Sity An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    is approximately: An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:    An aluminum cantilever beam of length L 5 0.65 m carries a distributed load, which includes its own weight, of intensity   . The beam cross section has a width of 50 mm and a height of 170 mm. Allowable bending stress is 95 MPa and allowable shear stress   The permissible value of load inten- Sity   is approximately:
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11
      (A) 0.5 (B) 0.7 (C) 1.2 (D) 1.5       (A) 0.5 (B) 0.7 (C) 1.2 (D) 1.5       (A) 0.5 (B) 0.7 (C) 1.2 (D) 1.5
(A) 0.5
(B) 0.7
(C) 1.2
(D) 1.5
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12
    68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses     68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses 68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:     68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses     68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses     68 mm, respectively. A bending moment is applied about the z axis resulting in a maximum stress in the aluminum of 55 MPa. The maximum stress in the steel is approximately:       Plane stress and strain; principal stresses Plane stress and strain; principal stresses
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13
A beam with an overhang is loaded by a uniform load of 3 kN/m over its entire length. Moment of iner- tia A beam with an overhang is loaded by a uniform load of 3 kN/m over its entire length. Moment of iner- tia   and distances to top and bottom of the beam cross section are 20 mm and 66.4 mm, Respectively. It is known that reactions at A and B are 4.5 kN and 13.5 kN, respectively. The maximum bending Stress in the beam is approximately:    and distances to top and bottom of the beam cross section are 20 mm and 66.4 mm,
Respectively. It is known that reactions at A and B are 4.5 kN and 13.5 kN, respectively. The maximum bending
Stress in the beam is approximately: A beam with an overhang is loaded by a uniform load of 3 kN/m over its entire length. Moment of iner- tia   and distances to top and bottom of the beam cross section are 20 mm and 66.4 mm, Respectively. It is known that reactions at A and B are 4.5 kN and 13.5 kN, respectively. The maximum bending Stress in the beam is approximately:    A beam with an overhang is loaded by a uniform load of 3 kN/m over its entire length. Moment of iner- tia   and distances to top and bottom of the beam cross section are 20 mm and 66.4 mm, Respectively. It is known that reactions at A and B are 4.5 kN and 13.5 kN, respectively. The maximum bending Stress in the beam is approximately:
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14
An aluminum light pole weighs 4300 N and supports an arm of weight 700 N, with the arm center of gravity at 1.2 m left of the centroidal axis of the pole. A wind force of 1500 N acts to the right at 7.5 m above
The base. The pole cross section at the base has an outside diameter of 235 mm and thickness of 20 mm. The
Maximum compressive stress at the base is approximately: An aluminum light pole weighs 4300 N and supports an arm of weight 700 N, with the arm center of gravity at 1.2 m left of the centroidal axis of the pole. A wind force of 1500 N acts to the right at 7.5 m above The base. The pole cross section at the base has an outside diameter of 235 mm and thickness of 20 mm. The Maximum compressive stress at the base is approximately:    An aluminum light pole weighs 4300 N and supports an arm of weight 700 N, with the arm center of gravity at 1.2 m left of the centroidal axis of the pole. A wind force of 1500 N acts to the right at 7.5 m above The base. The pole cross section at the base has an outside diameter of 235 mm and thickness of 20 mm. The Maximum compressive stress at the base is approximately:
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15
A copper wire (d 5 1.5 mm) is bent around a tube of radius R 5 0.6 m. The maximum normal strain in the wire is approximately: A copper wire (d 5 1.5 mm) is bent around a tube of radius R 5 0.6 m. The maximum normal strain in the wire is approximately:    A copper wire (d 5 1.5 mm) is bent around a tube of radius R 5 0.6 m. The maximum normal strain in the wire is approximately:
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