ARCH 264/564 Structural Elements Final exam May, 2007 Show all calculations. 1. Write the following number on the front cover of your exam booklet, top-left corner, above your name:
Solution: First, find the reduced live load based on the influence area, Ai = 48 x 32 = 1536 sq.ft. The reduction coefficient = 0.25 + 15 / (sq.rt. 1536) = 0.63, so the reduced live load = (.63)(75) = 47.25 psf.
From Table A-5.1 for Allowable Stress Design, the relevant load combinations to consider are as follows: Note that the load selected is the value shown in red, based on the bold-faced value representing the governing condition. In this case, they happen to be the same.
3. Wood beam design [15 points]. Design an indoor simply-supported wood girder with a 4-foot span supporting a single concentrated loads at the midpoint of the span. The concentrated load is 700#, of which 400# is live load and 300# is dead load. Assume Hem-Fir No.1 and assume dimension lumber. Design for bending; check for shear and live-load L/360 deflection. Do not redesign for shear or deflection. Do not use CH in shear check.
Solution: For Hem-Fir No. 1 (dimension lumber), Fb = 950 psi, Fv = 75 psi, and E = 1,500,000 psi. We can find the maximum bending moment and shear force as follows:
From Table A-4.1, select a 2x8 with S = 13.14 in3. Since CF = 1.05 (greater than 1.0) for the 2x8, it will work in bending, but a smaller cross-section with a larger CF might also work: check a 2x6 for bending:
2x6: With CF = 1.10, the adjusted allowable bending stress, F'b = 950(1.10)(1.0)(1.0) = 1045 psi, so the required section modulus, S = M / F'b = 8400 / 1045 = 8.04 in3. This is greater than the actual section modulus for the 2x6 (7.536 in3), so the 2x6 is no good for bending.
Select the 2x8 for bending.
Check for shear: The required area, A = 1.5(V / F'v) = 1.5(350 / 75) = 7 in2. Since the actual area, A = 10.88 in2 is greater or equal to the required area, the 2x8 is OK for shear.
Check for live load deflection: The allowable deflection = L/360 = 48"/360 = 0.13".
The actual deflection = CPL3 / (EI) where C = 35.94 (Table A-8.3 for concentrated load at midpoint), P = 400# (live load only), L = 4 feet, E = 1,500,000 psi, and I = 47.63 in4 (from Table A-4.1).
Actual deflection = 35.94(400)(43) / (1,500,000 x 47.63) = 0.01". Since the actual is smaller than the allowable, the 2x8 is OK for deflection.
4. Steel beam design [10 points]. Design a simply-supported, uniformly-loaded steel beam with a 40-foot span for bending only. The total distributed load, w = 1-1/2 kips per foot (or 1500 #/ft). Find the lightest W-section, assuming A-992 steel. Do not check for shear or deflection.
Solution: The allowable bending stress for A-992 steel (Table 3.12), Fb = 0.66Fy, where Fy = 50 ksi (Table A-3.11). Fb = 0.66(50) = 33 ksi. The maximum moment can be found as follows:
From Table A-8.4, select a W24x55 with S = 114 in3.
Solution: Based on equations in Table A-8.6.
Vc = 2(sq.rt.5000)(18 x 33) = 84,004# = 84 k.
Vs = (95.23 / 0.75) - 84 = 43 k.
s = 2(0.11)(60)(33) / 43 = 10.13". Round down to s = 10 inches.
b) Maximum spacing: Use smaller of: 7. Steel column analysis [10 points]. Find the capacity of a A-992 W21x101 steel column with both ends pinned (K = 1.0). The height is 15'.
Solution: From Table A-4.3, a W21x101 has these properties:
The slenderness ratio, kL / r = (1.0)(15 x 12) / 2.88 = 62.5 --> round up or down to 62 or 63 (rounding up is safer).
From Table A-7.4, using kL / r = 63, w get: Fa = 22.20 ksi.
The capacity, P = 22.20(29.8) = 662 k.
8. Reinforced concrete column design [15 points]. Find the required steel area and select 4 bars (if possible) for a rectangular 12"x16" column supporting a design load, Pu = 675 k with f'c = 5 ksi. Check if reinforcement ratio is within acceptable limits (1% and 8%).
Solution:
Pu = φα(0.85f'cAconc. + fyAs) where Aconc. = Agross - As. We can therefore write:
675 = (0.65 x 0.80)[0.85(5)(192 - As) + 60As]; solving for As, we get:
As = 8.65 in2. Select 4 No. 14 bars with As = 9.00 in2.
Check reinforcement ratio = 9.0 / 192 = 0.47 or 4.7% which is between 1% and 8%, so OK.
Solution:
The net area = Ag - (bolt hole area) = (5.5 x 19.5) - 3(5.5 x .75) = 107.25 - 12.375 = 94.875 in2. In this calculation, the bolt hole diameter is 1/8" larger than the bolt diameter, or 5/8" + 1/8" = 0.75". Three bolt holes are removed from the gross area, as shown in the sketch below: Last updated: 17 May, 2007 | ||||||||||