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Q2a) Member B is subjected to a compressive force of 800lb. if A and B are...
determine to the nearest ¼ in. the smallest dimension d of the support so that the average shear stress along section C does not exceed τ allow = 300 psi.
Member B is subjected to a compressive force of 650 lb. If A and B are both made of wood and are 3/8 in. thick, determine to the nearest ¼ in. the smallest dimension d of the support so that the average shear stress along section C does not exceed τ allow = 300 psi.
The flanged member shown below is subjected to an internal axial force of P = 6500...
The flanged member shown below is subjected to an internal axial force of P = 6500 lb, an internal shear force of V = 4500 lb, and an internal bending moment of M = 19200 lb-ft, acting in the directions shown. d M Iw y HI a y Ilk thu The dimensions of the cross section are: bf = 8.0 in. tp = 0.61 in. d = 11.0 in. tw = 0.38 in. The cross-sectional area of the flanged shape...
The plastic block is subjected to an axial compressive force of F 400 N. (Figure 1)...
The plastic block is subjected to an axial compressive force of F 400 N. (Figure 1) The caps at the top and bottom distribute the load uniformly throughout the block Part A Determine the average normal stress acting along section - Express your answer to three significant figures and include appropriate units. : Å Value RO? kPa 0.. = Sube Best - Part B Determine the average shear stress acting long section Express your answer to three significant figures and...
Consider a point in a structural member that is subjected to plane stress. Normal and shear...
Consider a point in a structural member that is subjected to plane stress. Normal and shear stress magnitudes acting on horizontal and vertical planes at the point are Sx = 51 ksi, Sy = 11 ksi, and Sxy = 32 ksi. (a) Determine the principal stresses (01 > 092) and the maximum In-plane shear stress Fruux acting at the point. (b) Find the smallest rotation angle 8, (counterclockwise is positive, clockwise is negative) that will rotate to principal directions. Then...
The walls are 10 in. thick with an allowable compressive stress of 300 psi (pounds per...
The walls are 10 in. thick with an allowable compressive stress of 300 psi (pounds per square inch). A 3 ft wide vertical strip of wall currently supports both a roof load of 1.5 kips and 11 floor loads of 2.0 kips per floor. Each story is 12 ft tall from floor to floor. The density of the masonry wall is 130 pcf (pounds per cubic foot). What is the maximum total force support by a 3ft wall segment for...
Please find the maximum applicable shear force on member a and member b. Then the required...
Please find the maximum applicable shear force on
member a and member b. Then the required spacing in the weaker
member such that both cross sections can support the same
maximum applicable
force as defined by the stronger member.
Having trouble with the equations and I'm not really
sure where I'm going wrong. Work would be appreciated. Thank
you!!
5 of 6 Learning Goal: To analyze two built-up members that have the same geometry but are fastened differently, determine the...
Consider a point in a structural member that is subjected to plane stress. Normal and shear...
Consider a point in a structural member that is subjected to
plane stress. Normal and shear stress magnitudes acting on
horizontal and vertical planes at the point are
Sx = 45 MPa, Sy = 10 MPa,
and Sxy = 36 MPa.
(a) Determine the principal stresses ( σ p 1 > σ p 2 ) and the
maximum in-plane shear stress τ max acting at the point.
(b) Find the smallest rotation angle θ p (counterclockwise is
positive, clockwise is...
Questions 5 through 11: FIG 2 shows member of width w and thickness subjected to a...
Questions 5 through 11: FIG 2 shows member of width w and thickness subjected to a tensile force P with two rectangular P glue joints. It is made of a single material with Young's modulus E and Poisson ratio v(shading is used to differentiate the three sections). (Q5 to Q6 1 point each, Q7 to Q11 2 points each) FIG 2 (Questions 5-11) 5) The average shear stress on joint 1 is a) 0 6) The average normal stress on...
P B A pressurized cylindrical air tank is subjected to a force P at a collar...
P B A pressurized cylindrical air tank is subjected to a force P at a collar B. The tank has an inner diameter (d = 160 mm) with wall thickness (1 = 6 mm). The gage pressure inside the tank is p = 5 MPa and the applied force is P = 9.5 kN. (a) Determine the maximum tensile stress o [MPa), maximum compressive stress oc [MPa] and maximum shear stress imax [MPa) at point a. (b) Repeat part (a)...
A tee-shaped flexural member is subjected to an internal axial force of P = 4,000 N,...
A tee-shaped flexural member is subjected to an internal axial
force of P = 4,000 N, an internal shear force of
V = 3500 N, and an internal bending moment of M =
1770 N-m, as shown. If the moment of inertia about the z
axis is 8,840,000 mm4 and the centroid of the section is
located 95 mm above the bottom surface of the beam, determine the
normal stress σy at point H.
-0.412 MPa
-0.615 MPa
0.000 MPa...
The flanged member shown below is subjected to an internal axial force of P = 6500 lb, an internal shear force of V = 4500 lb, and an internal bending moment of M = 19200 lb-ft, acting in the directions shown. d M Iw y HI a y Ilk thu The dimensions of the cross section are: bf = 8.0 in. tp = 0.61 in. d = 11.0 in. tw = 0.38 in. The cross-sectional area of the flanged shape...
The plastic block is subjected to an axial compressive force of F 400 N. (Figure 1) The caps at the top and bottom distribute the load uniformly throughout the block Part A Determine the average normal stress acting along section - Express your answer to three significant figures and include appropriate units. : Å Value RO? kPa 0.. = Sube Best - Part B Determine the average shear stress acting long section Express your answer to three significant figures and...
Consider a point in a structural member that is subjected to plane stress. Normal and shear stress magnitudes acting on horizontal and vertical planes at the point are Sx = 51 ksi, Sy = 11 ksi, and Sxy = 32 ksi. (a) Determine the principal stresses (01 > 092) and the maximum In-plane shear stress Fruux acting at the point. (b) Find the smallest rotation angle 8, (counterclockwise is positive, clockwise is negative) that will rotate to principal directions. Then...
Please find the maximum applicable shear force on
member a and member b. Then the required spacing in the weaker
member such that both cross sections can support the same
maximum applicable
force as defined by the stronger member.
Having trouble with the equations and I'm not really
sure where I'm going wrong. Work would be appreciated. Thank
you!!
5 of 6 Learning Goal: To analyze two built-up members that have the same geometry but are fastened differently, determine the...
Consider a point in a structural member that is subjected to
plane stress. Normal and shear stress magnitudes acting on
horizontal and vertical planes at the point are
Sx = 45 MPa, Sy = 10 MPa,
and Sxy = 36 MPa.
(a) Determine the principal stresses ( σ p 1 > σ p 2 ) and the
maximum in-plane shear stress τ max acting at the point.
(b) Find the smallest rotation angle θ p (counterclockwise is
positive, clockwise is...
Questions 5 through 11: FIG 2 shows member of width w and thickness subjected to a tensile force P with two rectangular P glue joints. It is made of a single material with Young's modulus E and Poisson ratio v(shading is used to differentiate the three sections). (Q5 to Q6 1 point each, Q7 to Q11 2 points each) FIG 2 (Questions 5-11) 5) The average shear stress on joint 1 is a) 0 6) The average normal stress on...
P B A pressurized cylindrical air tank is subjected to a force P at a collar B. The tank has an inner diameter (d = 160 mm) with wall thickness (1 = 6 mm). The gage pressure inside the tank is p = 5 MPa and the applied force is P = 9.5 kN. (a) Determine the maximum tensile stress o [MPa), maximum compressive stress oc [MPa] and maximum shear stress imax [MPa) at point a. (b) Repeat part (a)...
A tee-shaped flexural member is subjected to an internal axial
force of P = 4,000 N, an internal shear force of
V = 3500 N, and an internal bending moment of M =
1770 N-m, as shown. If the moment of inertia about the z
axis is 8,840,000 mm4 and the centroid of the section is
located 95 mm above the bottom surface of the beam, determine the
normal stress σy at point H.
-0.412 MPa
-0.615 MPa
0.000 MPa...
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