Deck 8: Axially Loaded Members

Full screen (f)
exit full mode
Question
       <div style=padding-top: 35px>        <div style=padding-top: 35px>        <div style=padding-top: 35px>        <div style=padding-top: 35px>
Use Space or
up arrow
down arrow
to flip the card.
Question
plane truss with span length L 5 4.5 m is constructed using cast iron pipes plane truss with span length L 5 4.5 m is constructed using cast iron pipes   with a cross-sectional area of   The displacement of joint B cannot exceed 2.7 mm. The maximum value of Loads P is approximately:   (A) 340 kN (B) 460 kN (C) 510 kN (D) 600 kN<div style=padding-top: 35px> with a cross-sectional area of plane truss with span length L 5 4.5 m is constructed using cast iron pipes   with a cross-sectional area of   The displacement of joint B cannot exceed 2.7 mm. The maximum value of Loads P is approximately:   (A) 340 kN (B) 460 kN (C) 510 kN (D) 600 kN<div style=padding-top: 35px> The displacement of joint B cannot exceed 2.7 mm. The maximum value of
Loads P is approximately: plane truss with span length L 5 4.5 m is constructed using cast iron pipes   with a cross-sectional area of   The displacement of joint B cannot exceed 2.7 mm. The maximum value of Loads P is approximately:   (A) 340 kN (B) 460 kN (C) 510 kN (D) 600 kN<div style=padding-top: 35px>
(A) 340 kN
(B) 460 kN
(C) 510 kN
(D) 600 kN
Question
wires, one copper and the other steel, of equal length stretch the same amount under an applied load P. The moduli of elasticity for each is wires, one copper and the other steel, of equal length stretch the same amount under an applied load P. The moduli of elasticity for each is   GPa. The ratio of the diameter of the copper Wire to that of the steel wire is approximately:   (A) 1.00 (B) 1.08 (C) 1.19 (D) 1.32<div style=padding-top: 35px> GPa. The ratio of the diameter of the copper
Wire to that of the steel wire is approximately: wires, one copper and the other steel, of equal length stretch the same amount under an applied load P. The moduli of elasticity for each is   GPa. The ratio of the diameter of the copper Wire to that of the steel wire is approximately:   (A) 1.00 (B) 1.08 (C) 1.19 (D) 1.32<div style=padding-top: 35px>
(A) 1.00
(B) 1.08
(C) 1.19
(D) 1.32
Question
A copper bar (d 5 10 mm, E 5 110 GPa) is loaded by tensile load P 5 11.5 kN. The maximum shear stress in the bar is approximately: A copper bar (d 5 10 mm, E 5 110 GPa) is loaded by tensile load P 5 11.5 kN. The maximum shear stress in the bar is approximately:    <div style=padding-top: 35px> A copper bar (d 5 10 mm, E 5 110 GPa) is loaded by tensile load P 5 11.5 kN. The maximum shear stress in the bar is approximately:    <div style=padding-top: 35px>
Question
A steel bolt (area A steel bolt (area   is enclosed by a copper tube (length 5 0.5 m, area 5   110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately:    <div style=padding-top: 35px> is enclosed by a copper tube (length 5 0.5 m, area 5 A steel bolt (area   is enclosed by a copper tube (length 5 0.5 m, area 5   110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately:    <div style=padding-top: 35px> 110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately: A steel bolt (area   is enclosed by a copper tube (length 5 0.5 m, area 5   110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately:    <div style=padding-top: 35px> A steel bolt (area   is enclosed by a copper tube (length 5 0.5 m, area 5   110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately:    <div style=padding-top: 35px>
Question
A steel plane truss is loaded at B and C by forces P 5 200 kN. The cross-sectional area of each member A steel plane truss is loaded at B and C by forces P 5 200 kN. The cross-sectional area of each member   . Truss dimensions are H 5 3 m and L 5 4 m. The maximum shear stress in bar AB is approx- imately:    <div style=padding-top: 35px> . Truss dimensions are H 5 3 m and L 5 4 m. The maximum shear stress in bar AB is approx- imately: A steel plane truss is loaded at B and C by forces P 5 200 kN. The cross-sectional area of each member   . Truss dimensions are H 5 3 m and L 5 4 m. The maximum shear stress in bar AB is approx- imately:    <div style=padding-top: 35px> A steel plane truss is loaded at B and C by forces P 5 200 kN. The cross-sectional area of each member   . Truss dimensions are H 5 3 m and L 5 4 m. The maximum shear stress in bar AB is approx- imately:    <div style=padding-top: 35px>
Question
nylon bar (E 5 2.1 GPa) with diameter 12 mm, length 4.5 m, and weight 5.6 N hangs vertically under its own weight. The elongation of the bar at its free end is approximately: nylon bar (E 5 2.1 GPa) with diameter 12 mm, length 4.5 m, and weight 5.6 N hangs vertically under its own weight. The elongation of the bar at its free end is approximately:   (A) 0.05 mm (B) 0.07 mm (C) 0.11 mm (D) 0.17 mm<div style=padding-top: 35px>
(A) 0.05 mm
(B) 0.07 mm
(C) 0.11 mm
(D) 0.17 mm
Question
brass bar (E 5 110 MPa) of length brass bar (E 5 110 MPa) of length   18 mm over one-half of its length and   18 mm over the other half. Compare this nonprismatic bar to a prismatic bar of the same volume of material with constant diameter d and length L. The elongation of the prismatic bar under the same load P 5 25 kN is approximately:   (A) 3 mm (B) 4 mm (C) 5 mm (D) 6 mm<div style=padding-top: 35px> 18 mm over one-half of its length and brass bar (E 5 110 MPa) of length   18 mm over one-half of its length and   18 mm over the other half. Compare this nonprismatic bar to a prismatic bar of the same volume of material with constant diameter d and length L. The elongation of the prismatic bar under the same load P 5 25 kN is approximately:   (A) 3 mm (B) 4 mm (C) 5 mm (D) 6 mm<div style=padding-top: 35px> 18 mm over the other half. Compare this nonprismatic bar to a prismatic bar of the same volume of material with constant diameter d and length L. The elongation of the prismatic bar under the same load
P 5 25 kN is approximately: brass bar (E 5 110 MPa) of length   18 mm over one-half of its length and   18 mm over the other half. Compare this nonprismatic bar to a prismatic bar of the same volume of material with constant diameter d and length L. The elongation of the prismatic bar under the same load P 5 25 kN is approximately:   (A) 3 mm (B) 4 mm (C) 5 mm (D) 6 mm<div style=padding-top: 35px>
(A) 3 mm
(B) 4 mm
(C) 5 mm
(D) 6 mm
Question
nonprismatic cantilever bar has an internal cylindrical hole of diameter nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    <div style=padding-top: 35px> /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4) nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    <div style=padding-top: 35px> nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    <div style=padding-top: 35px> /2 is applied at x 5 L. Assume
That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the
Free end is: nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    <div style=padding-top: 35px> nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    <div style=padding-top: 35px>
Question
A brass wire (d 5 2.0 mm, E 5 110 GPa) is pretensioned to T 5 85 N. The coefficient of thermal expan- sion for the wire is 19.5 A brass wire (d 5 2.0 mm, E 5 110 GPa) is pretensioned to T 5 85 N. The coefficient of thermal expan- sion for the wire is 19.5   /°C. The temperature change at which the wire goes slack is approximately:    <div style=padding-top: 35px> /°C. The temperature change at which the wire goes slack is approximately: A brass wire (d 5 2.0 mm, E 5 110 GPa) is pretensioned to T 5 85 N. The coefficient of thermal expan- sion for the wire is 19.5   /°C. The temperature change at which the wire goes slack is approximately:    <div style=padding-top: 35px> A brass wire (d 5 2.0 mm, E 5 110 GPa) is pretensioned to T 5 85 N. The coefficient of thermal expan- sion for the wire is 19.5   /°C. The temperature change at which the wire goes slack is approximately:    <div style=padding-top: 35px>
Question
      (A) 0.9 mm (B) 1.6 mm (C) 2.1 mm (D) 3.4 mm<div style=padding-top: 35px>       (A) 0.9 mm (B) 1.6 mm (C) 2.1 mm (D) 3.4 mm<div style=padding-top: 35px>       (A) 0.9 mm (B) 1.6 mm (C) 2.1 mm (D) 3.4 mm<div style=padding-top: 35px>
(A) 0.9 mm
(B) 1.6 mm
(C) 2.1 mm
(D) 3.4 mm
Question
       <div style=padding-top: 35px>        <div style=padding-top: 35px>        <div style=padding-top: 35px>        <div style=padding-top: 35px>
Question
A plane stress element on a bar in uniaxial stress has a tensile stress of A plane stress element on a bar in uniaxial stress has a tensile stress of   78 MPa (see figure). The maximum shear stress in the bar is approximately:    <div style=padding-top: 35px> 78 MPa (see figure). The maximum shear stress in the bar is approximately: A plane stress element on a bar in uniaxial stress has a tensile stress of   78 MPa (see figure). The maximum shear stress in the bar is approximately:    <div style=padding-top: 35px> A plane stress element on a bar in uniaxial stress has a tensile stress of   78 MPa (see figure). The maximum shear stress in the bar is approximately:    <div style=padding-top: 35px>
Question
A prismatic bar (diameter A prismatic bar (diameter       Torsional stresses and deformations; power transmission (A) 0.9 (B) 1.2 (C) 1.4 (D) 2.1<div style=padding-top: 35px> A prismatic bar (diameter       Torsional stresses and deformations; power transmission (A) 0.9 (B) 1.2 (C) 1.4 (D) 2.1<div style=padding-top: 35px> A prismatic bar (diameter       Torsional stresses and deformations; power transmission (A) 0.9 (B) 1.2 (C) 1.4 (D) 2.1<div style=padding-top: 35px> Torsional stresses and deformations; power transmission
(A) 0.9
(B) 1.2
(C) 1.4
(D) 2.1
Question
A steel bar of rectangular cross section (a 5 38 mm, b 5 50 mm) carries a tensile load P. The allowable stresses in tension and shear are 100 MPa and 48 MPa, respectively. The maximum permissible load A steel bar of rectangular cross section (a 5 38 mm, b 5 50 mm) carries a tensile load P. The allowable stresses in tension and shear are 100 MPa and 48 MPa, respectively. The maximum permissible load   is Approximately:    <div style=padding-top: 35px> is
Approximately: A steel bar of rectangular cross section (a 5 38 mm, b 5 50 mm) carries a tensile load P. The allowable stresses in tension and shear are 100 MPa and 48 MPa, respectively. The maximum permissible load   is Approximately:    <div style=padding-top: 35px> A steel bar of rectangular cross section (a 5 38 mm, b 5 50 mm) carries a tensile load P. The allowable stresses in tension and shear are 100 MPa and 48 MPa, respectively. The maximum permissible load   is Approximately:    <div style=padding-top: 35px>
Question
  Initially, both shell and core have a length of 100 mm. A load P is applied to both shell and core through a cap plate. The load P required to compress both shell and core by 0.10 mm is approximately:   (A) 10.2 kN (B) 13.4 kN (C) 18.5 kN (D) 21.0 kN<div style=padding-top: 35px> Initially, both shell and core have a length of 100 mm. A load P is applied to both shell and core through a cap plate. The load P required to compress both shell and core by 0.10 mm is approximately:   Initially, both shell and core have a length of 100 mm. A load P is applied to both shell and core through a cap plate. The load P required to compress both shell and core by 0.10 mm is approximately:   (A) 10.2 kN (B) 13.4 kN (C) 18.5 kN (D) 21.0 kN<div style=padding-top: 35px>
(A) 10.2 kN
(B) 13.4 kN
(C) 18.5 kN
(D) 21.0 kN
Unlock Deck
Sign up to unlock the cards in this deck!
Unlock Deck
Unlock Deck
1/16
auto play flashcards
Play
simple tutorial
Full screen (f)
exit full mode
Deck 8: Axially Loaded Members
1
C
2
plane truss with span length L 5 4.5 m is constructed using cast iron pipes plane truss with span length L 5 4.5 m is constructed using cast iron pipes   with a cross-sectional area of   The displacement of joint B cannot exceed 2.7 mm. The maximum value of Loads P is approximately:   (A) 340 kN (B) 460 kN (C) 510 kN (D) 600 kN with a cross-sectional area of plane truss with span length L 5 4.5 m is constructed using cast iron pipes   with a cross-sectional area of   The displacement of joint B cannot exceed 2.7 mm. The maximum value of Loads P is approximately:   (A) 340 kN (B) 460 kN (C) 510 kN (D) 600 kN The displacement of joint B cannot exceed 2.7 mm. The maximum value of
Loads P is approximately: plane truss with span length L 5 4.5 m is constructed using cast iron pipes   with a cross-sectional area of   The displacement of joint B cannot exceed 2.7 mm. The maximum value of Loads P is approximately:   (A) 340 kN (B) 460 kN (C) 510 kN (D) 600 kN
(A) 340 kN
(B) 460 kN
(C) 510 kN
(D) 600 kN
B
3
wires, one copper and the other steel, of equal length stretch the same amount under an applied load P. The moduli of elasticity for each is wires, one copper and the other steel, of equal length stretch the same amount under an applied load P. The moduli of elasticity for each is   GPa. The ratio of the diameter of the copper Wire to that of the steel wire is approximately:   (A) 1.00 (B) 1.08 (C) 1.19 (D) 1.32 GPa. The ratio of the diameter of the copper
Wire to that of the steel wire is approximately: wires, one copper and the other steel, of equal length stretch the same amount under an applied load P. The moduli of elasticity for each is   GPa. The ratio of the diameter of the copper Wire to that of the steel wire is approximately:   (A) 1.00 (B) 1.08 (C) 1.19 (D) 1.32
(A) 1.00
(B) 1.08
(C) 1.19
(D) 1.32
D
4
A copper bar (d 5 10 mm, E 5 110 GPa) is loaded by tensile load P 5 11.5 kN. The maximum shear stress in the bar is approximately: A copper bar (d 5 10 mm, E 5 110 GPa) is loaded by tensile load P 5 11.5 kN. The maximum shear stress in the bar is approximately:    A copper bar (d 5 10 mm, E 5 110 GPa) is loaded by tensile load P 5 11.5 kN. The maximum shear stress in the bar is approximately:
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
5
A steel bolt (area A steel bolt (area   is enclosed by a copper tube (length 5 0.5 m, area 5   110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately:    is enclosed by a copper tube (length 5 0.5 m, area 5 A steel bolt (area   is enclosed by a copper tube (length 5 0.5 m, area 5   110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately:    110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately: A steel bolt (area   is enclosed by a copper tube (length 5 0.5 m, area 5   110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately:    A steel bolt (area   is enclosed by a copper tube (length 5 0.5 m, area 5   110 GPa) and the end nut is turned until it is just snug. The pitch of the bolt threads is 1.25 mm. The bolt is now tightened by a quarter turn of the nut. The resulting stress in the bolt is approximately:
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
6
A steel plane truss is loaded at B and C by forces P 5 200 kN. The cross-sectional area of each member A steel plane truss is loaded at B and C by forces P 5 200 kN. The cross-sectional area of each member   . Truss dimensions are H 5 3 m and L 5 4 m. The maximum shear stress in bar AB is approx- imately:    . Truss dimensions are H 5 3 m and L 5 4 m. The maximum shear stress in bar AB is approx- imately: A steel plane truss is loaded at B and C by forces P 5 200 kN. The cross-sectional area of each member   . Truss dimensions are H 5 3 m and L 5 4 m. The maximum shear stress in bar AB is approx- imately:    A steel plane truss is loaded at B and C by forces P 5 200 kN. The cross-sectional area of each member   . Truss dimensions are H 5 3 m and L 5 4 m. The maximum shear stress in bar AB is approx- imately:
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
7
nylon bar (E 5 2.1 GPa) with diameter 12 mm, length 4.5 m, and weight 5.6 N hangs vertically under its own weight. The elongation of the bar at its free end is approximately: nylon bar (E 5 2.1 GPa) with diameter 12 mm, length 4.5 m, and weight 5.6 N hangs vertically under its own weight. The elongation of the bar at its free end is approximately:   (A) 0.05 mm (B) 0.07 mm (C) 0.11 mm (D) 0.17 mm
(A) 0.05 mm
(B) 0.07 mm
(C) 0.11 mm
(D) 0.17 mm
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
8
brass bar (E 5 110 MPa) of length brass bar (E 5 110 MPa) of length   18 mm over one-half of its length and   18 mm over the other half. Compare this nonprismatic bar to a prismatic bar of the same volume of material with constant diameter d and length L. The elongation of the prismatic bar under the same load P 5 25 kN is approximately:   (A) 3 mm (B) 4 mm (C) 5 mm (D) 6 mm 18 mm over one-half of its length and brass bar (E 5 110 MPa) of length   18 mm over one-half of its length and   18 mm over the other half. Compare this nonprismatic bar to a prismatic bar of the same volume of material with constant diameter d and length L. The elongation of the prismatic bar under the same load P 5 25 kN is approximately:   (A) 3 mm (B) 4 mm (C) 5 mm (D) 6 mm 18 mm over the other half. Compare this nonprismatic bar to a prismatic bar of the same volume of material with constant diameter d and length L. The elongation of the prismatic bar under the same load
P 5 25 kN is approximately: brass bar (E 5 110 MPa) of length   18 mm over one-half of its length and   18 mm over the other half. Compare this nonprismatic bar to a prismatic bar of the same volume of material with constant diameter d and length L. The elongation of the prismatic bar under the same load P 5 25 kN is approximately:   (A) 3 mm (B) 4 mm (C) 5 mm (D) 6 mm
(A) 3 mm
(B) 4 mm
(C) 5 mm
(D) 6 mm
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
9
nonprismatic cantilever bar has an internal cylindrical hole of diameter nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4) nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    /2 is applied at x 5 L. Assume
That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the
Free end is: nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:    nonprismatic cantilever bar has an internal cylindrical hole of diameter   /2 from 0 to x, so the net area of the cross section for Segment 1 is (3/4)     /2 is applied at x 5 L. Assume That E is constant. The length of the hollow segment, x, required to obtain axial displacement δ 5 PL/EA at the Free end is:
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
10
A brass wire (d 5 2.0 mm, E 5 110 GPa) is pretensioned to T 5 85 N. The coefficient of thermal expan- sion for the wire is 19.5 A brass wire (d 5 2.0 mm, E 5 110 GPa) is pretensioned to T 5 85 N. The coefficient of thermal expan- sion for the wire is 19.5   /°C. The temperature change at which the wire goes slack is approximately:    /°C. The temperature change at which the wire goes slack is approximately: A brass wire (d 5 2.0 mm, E 5 110 GPa) is pretensioned to T 5 85 N. The coefficient of thermal expan- sion for the wire is 19.5   /°C. The temperature change at which the wire goes slack is approximately:    A brass wire (d 5 2.0 mm, E 5 110 GPa) is pretensioned to T 5 85 N. The coefficient of thermal expan- sion for the wire is 19.5   /°C. The temperature change at which the wire goes slack is approximately:
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
11
      (A) 0.9 mm (B) 1.6 mm (C) 2.1 mm (D) 3.4 mm       (A) 0.9 mm (B) 1.6 mm (C) 2.1 mm (D) 3.4 mm       (A) 0.9 mm (B) 1.6 mm (C) 2.1 mm (D) 3.4 mm
(A) 0.9 mm
(B) 1.6 mm
(C) 2.1 mm
(D) 3.4 mm
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
12
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
13
A plane stress element on a bar in uniaxial stress has a tensile stress of A plane stress element on a bar in uniaxial stress has a tensile stress of   78 MPa (see figure). The maximum shear stress in the bar is approximately:    78 MPa (see figure). The maximum shear stress in the bar is approximately: A plane stress element on a bar in uniaxial stress has a tensile stress of   78 MPa (see figure). The maximum shear stress in the bar is approximately:    A plane stress element on a bar in uniaxial stress has a tensile stress of   78 MPa (see figure). The maximum shear stress in the bar is approximately:
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
14
A prismatic bar (diameter A prismatic bar (diameter       Torsional stresses and deformations; power transmission (A) 0.9 (B) 1.2 (C) 1.4 (D) 2.1 A prismatic bar (diameter       Torsional stresses and deformations; power transmission (A) 0.9 (B) 1.2 (C) 1.4 (D) 2.1 A prismatic bar (diameter       Torsional stresses and deformations; power transmission (A) 0.9 (B) 1.2 (C) 1.4 (D) 2.1 Torsional stresses and deformations; power transmission
(A) 0.9
(B) 1.2
(C) 1.4
(D) 2.1
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
15
A steel bar of rectangular cross section (a 5 38 mm, b 5 50 mm) carries a tensile load P. The allowable stresses in tension and shear are 100 MPa and 48 MPa, respectively. The maximum permissible load A steel bar of rectangular cross section (a 5 38 mm, b 5 50 mm) carries a tensile load P. The allowable stresses in tension and shear are 100 MPa and 48 MPa, respectively. The maximum permissible load   is Approximately:    is
Approximately: A steel bar of rectangular cross section (a 5 38 mm, b 5 50 mm) carries a tensile load P. The allowable stresses in tension and shear are 100 MPa and 48 MPa, respectively. The maximum permissible load   is Approximately:    A steel bar of rectangular cross section (a 5 38 mm, b 5 50 mm) carries a tensile load P. The allowable stresses in tension and shear are 100 MPa and 48 MPa, respectively. The maximum permissible load   is Approximately:
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
16
  Initially, both shell and core have a length of 100 mm. A load P is applied to both shell and core through a cap plate. The load P required to compress both shell and core by 0.10 mm is approximately:   (A) 10.2 kN (B) 13.4 kN (C) 18.5 kN (D) 21.0 kN Initially, both shell and core have a length of 100 mm. A load P is applied to both shell and core through a cap plate. The load P required to compress both shell and core by 0.10 mm is approximately:   Initially, both shell and core have a length of 100 mm. A load P is applied to both shell and core through a cap plate. The load P required to compress both shell and core by 0.10 mm is approximately:   (A) 10.2 kN (B) 13.4 kN (C) 18.5 kN (D) 21.0 kN
(A) 10.2 kN
(B) 13.4 kN
(C) 18.5 kN
(D) 21.0 kN
Unlock Deck
Unlock for access to all 16 flashcards in this deck.
Unlock Deck
k this deck
locked card icon
Unlock Deck
Unlock for access to all 16 flashcards in this deck.