Errata for “Structural Steel Design,” Fourth Edition, by Jack C ...
Errata for “Structural Steel Design,” Fourth Edition, by Jack C ...
Errata for “Structural Steel Design,” Fourth Edition, by Jack C ...
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<strong>Errata</strong> <strong>for</strong> <strong>“Structural</strong> <strong>Steel</strong> <strong>Design</strong>,<strong>”</strong> <strong>Fourth</strong> <strong>Edition</strong>, <strong>by</strong> <strong>Jack</strong> C. McCormac<br />
Page 1 of 6<br />
Updated 03-Oct-12<br />
Chapter 4<br />
1. On page 102, in the first paragraph, the reference to the AISC Specification should be<br />
D1 (not D.1).<br />
2. On page 106, Example 4-1, in the calculation <strong>for</strong> “min Ag<strong>”</strong>, a value of 0.380 (not 0.520)<br />
should be used in the estimated area <strong>for</strong> the bolt holes. The subsequent value <strong>for</strong> “min<br />
Ag<strong>”</strong> should be 9.09 in 2 (not 9.65 in 2 ). The value 0.380 is noted in the first paragraph of<br />
page 106, however a value of 0.520 is used in the calculation.<br />
3. On page 111, Example 4-3, the problem states that the connection of the tension<br />
member is through the channel flanges. However, in the calculation <strong>for</strong> U (on page 112),<br />
the x distance is taken from the back of the channel web to the centroid of the channel<br />
implying that the connection plane is to the web and not the flange.<br />
To determine U <strong>for</strong> a connection to the flanges, an approximate value y (i.e. the<br />
distance from the top of the top flange to the centroid of the half-channel) can be<br />
determined assuming the flange and web are rectangles. Based on such an assumption,<br />
the approximate location of y <strong>for</strong> the centroid of the half channel is 2.17" below the top<br />
of the top flange giving a value <strong>for</strong> U = 1 - 2.17/6 = 0.638. As a result, the member is not<br />
adequate <strong>for</strong> the given loads based on tensile rupture strength.<br />
In the given problem statement if the connection is to the web, then the calculation<br />
shown <strong>for</strong> U can be preserved and the section is adequate.<br />
Figure 4-02 may be retained in the example. This figure shows the location of the<br />
bolt holes that are used <strong>for</strong> the tie plates and the corresponding gage distance which is<br />
used in the example <strong>for</strong> the design of the tie plate. However, these bolt holes would not<br />
be the holes <strong>for</strong> the bolted connection to another member.<br />
Chapter 6<br />
1. On page 198, Problem 6-21, the steel should be specified as 36 ksi, not 50 ksi. Angles<br />
are usually furnished in A36 steel. The answer furnished <strong>by</strong> the author is based on 36<br />
ksi.<br />
Chapter 10<br />
1. On page 297, Example 10-1 (Part b), the positive moment values shown in the moment<br />
diagram are based on the ASD critical load combination and should be 263 (not 600),<br />
295 (not 695), and 233 (not 446).<br />
Furthermore, on page 297, the values of moment used in the equation to determine<br />
the maximum positive moment <strong>for</strong> design should be 295 (not 695). The resulting<br />
maximum positive moment <strong>for</strong> design should be +345.5 ft-k (not +745.5 ft-k).<br />
2. On page 321, Example 10-7, <strong>for</strong> the LRFD solution, the second term in the equation <strong>for</strong><br />
wux should be “1.6 S<strong>”</strong> not the number “1.65.<strong>”</strong> The following calculations are correct.<br />
3. On page 321, Example 10-7, <strong>for</strong> the ASD solution, the second term in the equation <strong>for</strong><br />
wax should be “S<strong>”</strong> not the number “5.<strong>”</strong> The following calculations are correct.<br />
4. On page 329, in the fourth line of the first paragraph, the term “φcPp<strong>”</strong> should be replaced<br />
with “φc0.85f’c<strong>”</strong> and the term “Pp/Ωc<strong>”</strong> should be replaced with the term “0.85f’c/Ωc.<strong>”</strong>
5. On page 329, the equations <strong>for</strong> A1 that follow the first paragraph should be corrected as<br />
follows.<br />
A1 = Ru/φc0.85f’c A1 = ΩcRa/0.85f’c<br />
6. On page 329, Example 10-10, the value of Fyw used to check web local yielding should<br />
be 50 ksi (the steel <strong>for</strong> the beam) not 36 ksi (the steel <strong>for</strong> the plate). The resulting value<br />
<strong>for</strong> Rn should be 272.9 kips (not 196.5 kips).<br />
Furthermore, the value used <strong>for</strong> Rn in the subsequent LRFD and ASD calculations on<br />
page 330 should be 272.9 kips (not 196.5 kips). φRn should be 272.9 kips (not 196.5<br />
kips) and Rn/Ω should be 181.9 kips (not 131 kips).<br />
The A36 steel is specified <strong>for</strong> the plate steel. The steel used <strong>for</strong> the beam should be<br />
A992 (Fy = 50 ksi).<br />
7. On page 330, Example 10-10, the value of Fyw used to check web crippling should be 50<br />
ksi (the steel <strong>for</strong> the beam) not 36 ksi (the steel used <strong>for</strong> the plate). The resulting value<br />
<strong>for</strong> Rn should be 261.3 kips (not 221.7 kips).<br />
Furthermore, the value used <strong>for</strong> Rn in the subsequent LRFD and ASD calculations on<br />
page 330 should be 261.3 kips (not 221.7 kips). φRn should be 196.0 kips (not 166 kips)<br />
and Rn/Ω should be 130.6 kips (not 111 kips).<br />
The A36 steel is specified <strong>for</strong> the plate steel. The steel used <strong>for</strong> the beam should be<br />
A992 (Fy = 50 ksi).<br />
8. On page 331, in the LRFD and ASD calculations <strong>for</strong> thickness, the value of Fy should be<br />
50 ksi (not 36 ksi) since the steel used <strong>for</strong> the beam should be A992 (Fy = 50 ksi). The<br />
resulting required plate thickness should be 0.758<strong>”</strong> <strong>for</strong> LRFD and 0.772<strong>”</strong> <strong>for</strong> ASD. As a<br />
result, both calculated thicknesses are less than the flange thickness of 0.810<strong>”</strong> <strong>for</strong> the<br />
W18 x 71.<br />
Furthermore, the area A1 provided <strong>by</strong> the flange is 8 x 7.64 = 61.12 in 2 and is less<br />
than the required area A1 of 75.8 in 2 (LRFD) or 78.43 in 2 (ASD) computed on page<br />
329.Thus the stresses in the concrete would exceed the allowable stresses if the flange<br />
alone were used <strong>for</strong> bearing without a bearing plate.<br />
Chapter 11<br />
1. On page 346, in the notation <strong>for</strong> AISC Equation C2-6b, the term <strong>for</strong> “first-order interstory<br />
drift due to ∑H lateral <strong>for</strong>ces<strong>”</strong> should be “ΔH<strong>”</strong> (not “ΔH<strong>”</strong>). The error occurs in the equation<br />
and in the following list where the factors are defined.<br />
2. On page 354, Example 11-5, near the bottom of the page in the LRFD calculations <strong>for</strong><br />
the equation ½ρPr + (9/8)(bxMrx + <strong>by</strong>Mry) ≤ 1.0, the value used <strong>for</strong> Pr should be “244<strong>”</strong> (not<br />
“???3.244<strong>”</strong>).<br />
Furthermore, the value used <strong>for</strong> <strong>by</strong> should be 2.32 x 10 -3 (not (2.3 x 10 -3 ).<br />
The answer 0.742 appears to be correct.<br />
3. On page 360, Example 11-9, in the given in<strong>for</strong>mation, the notation ∑Pu = 5000 k should<br />
be ∑Pnt = 5000 k, the notation ∑Pex = 40,000 k should be ∑Pe2x = 40,000 k, and the<br />
notation ∑Pey = 5000 k should be ∑Pe2y = 5000 k.<br />
Furthermore, on page 361, the value used <strong>for</strong> Pr in the calculation <strong>for</strong> Pr/Pc should be<br />
286 (not 250) and the result of the calculation should be 0.238 (not 0.208).<br />
Page 2 of 6
Furthermore, on page 361, the value used <strong>for</strong> Pr in the calculation <strong>for</strong> B1x should be<br />
286 (not 250). The result of the calculation appears to be correct.<br />
Furthermore, on page 361, the value used <strong>for</strong> Pr in the calculation <strong>for</strong> B1y should be<br />
286 (not 250). The result of the calculation should be 0.215 (not 0.213).<br />
4. On page 362, Problem 11-10, the value <strong>for</strong> Cmx should be 1.0 (not 0.85). A value <strong>for</strong> Cmy<br />
is not required.<br />
5. On page 343, at the end of the second paragraph <strong>for</strong> Section 11.3, the notation <strong>for</strong> the<br />
secondary moment produced due to sidesway should be PntΔ (not Mlt).<br />
6. On page 362, Problem 11-10, Cmx = 1.0 (not 0.85) and Cmy (listed as 0.85) is not<br />
required.<br />
Chapter 12<br />
1. On page 388, Example 12-1, the reference following the calculation <strong>for</strong> the effective area<br />
Ae should be AISC Spec. J4.1 (not AISC Spec. J4.16).<br />
2. On page 396, Example 12-4, the values actually used in the example <strong>for</strong> PD is 30 kips<br />
and <strong>for</strong> PL is 50 kips (not 50 kips and 30 kips, respectively, as listed in the given<br />
in<strong>for</strong>mation).<br />
3. On page 397, Example 12-4, in the calculation <strong>for</strong> the bearing strength of the 6 bolts, the<br />
coefficient used to determine the bearing strength Rn should be 1.2 (not 1.5) since<br />
de<strong>for</strong>mation around the bolt holes was listed as a design concern in the problem<br />
statement. The resulting value <strong>for</strong> Rn should be 347.2 kips (not 434 kips).<br />
Furthermore, the value used <strong>for</strong> Rn in the subsequent LRFD and ASD calculations on<br />
page 398 should be 347.2 kips (not 434 kips). φRn should be 260 kips (not 326 kips) and<br />
Rn/Ω should be 173.6 kips (not 217 kips).<br />
Chapter 13<br />
1. On page 420, Example 13-4, the problem states that de<strong>for</strong>mations at bolt holes at<br />
service loads is not a design consideration. Consequently, the second part of the<br />
equation used to determine the nominal bearing strength should be “3.0 d t Fu<strong>”</strong> (rather<br />
than “2.4 d t Fu<strong>”</strong>).<br />
Chapter 14<br />
1. On page 466, Table 14.2, the minimum size of fillet welds is based on the material<br />
thickness of the “thinner<strong>”</strong> (not “thicker<strong>”</strong>) part joined per AISC Table J2.4.<br />
2. On page 471, the calculations to check the tensile rupture strength of the connecting<br />
elements should be as follows.<br />
From Table 3.2 (p. 75 of the textbook), Case 4:<br />
1.5w = 1.5(8) = 12<strong>”</strong> > ℓ = 10<strong>”</strong> > w = 8<strong>”</strong>, thus U = 0.75<br />
An = (3/4)(10) = 7.5 in 2<br />
Ae = U An = 0.75 (7.5) = 5.625 in 2 (not 10.5 in 2 )<br />
Rn = Fu Ae = 65 (5.625) = 365.6 kips (not 682.5 kips)<br />
Furthermore, the value used <strong>for</strong> Rn in the subsequent LRFD and ASD calculations on<br />
page 471 should be 365.6 kips (not 682.5 kips). φRn should be 274.2 kips (not 511.9<br />
kips) and Rn/Ω should be 182.8 kips (not 341.2 kips).<br />
Page 3 of 6
3. On page 476, in the paragraph following the equation <strong>for</strong> FwAw/Ω, the first line should<br />
read “For LRFD with E70 electrodes, φRn = (0.0199)(70) = 1.39 k/in.<strong>”</strong> The φ term is<br />
omitted in the text.<br />
4. On page 481, Example 14-7, the length of the slot weld is determined to be 6<strong>”</strong> (LRFD)<br />
and 6.5<strong>”</strong> (ASD). However, the maximum length of the slot weld is 5<strong>”</strong>.<br />
5. On page 493, in the first line of the second paragraph, the words “and 14-13<strong>”</strong> should be<br />
deleted. There is no Example 14-13 in the text.<br />
6. On page 493, in the first line of the third paragraph, the words “two W sections<strong>”</strong> should<br />
be replaced with “two plates.<strong>”</strong> Example 14-12 specifies two plates.<br />
Chapter 15<br />
1. On page 519, Example 15-3, under “Select Weld B <strong>for</strong> column,<strong>”</strong> the thickness of the<br />
column flange <strong>for</strong> the W14 x 61 is 0.645<strong>”</strong> (not 0.545<strong>”</strong>).<br />
Furthermore, in the last line of Example 15-3, where the angles are specified, the<br />
angle thickness should be 3/8<strong>”</strong> (not 5/16<strong>”</strong>). A minimum angle thickness of 3/8<strong>”</strong> was<br />
determined earlier in the example.<br />
2. On page 522, in the next to last paragraph <strong>for</strong> Example 15-4, the 5 inch dimension was<br />
determined from page 10-101 of the AISC Manual (not page 10-10).<br />
3. On page 524, Example 15-5, under the check <strong>for</strong> local web yielding, the reference<br />
should be to AISC Equation J10-3 (not AISC Equation J10-2).<br />
3. On page 525, the angle that is specified is L8 x 4 x 7/16 x 0 ft 8 in <strong>for</strong> both LRFD and<br />
ASD. However, this angle thickness is outside the range of available angle thicknesses<br />
listed in AISC Table 10-6 <strong>for</strong> the 8 x 4 angle. The angle thickness should be 3/4<strong>”</strong> (not<br />
7/16<strong>”</strong>).<br />
Furthermore, based on an examination of Table 10-6 with N = 1½<strong>”</strong>, the required<br />
angle thickness is 3/4<strong>”</strong> <strong>for</strong> LRFD and ASD.<br />
Furthermore, in the ASD calculations to determine the angle thickness t, the ASD<br />
notation should be Rn/Ω (not Rn/φ).<br />
4. On page 531, rule number 2 should be stated as follows: “The stiffener thickness should<br />
not be less than one-half the thickness of the flange (tf/2) or half the thickness of the<br />
moment connection plate delivering the concentrated load, and not less than the width<br />
divided <strong>by</strong> 15.<strong>”</strong> (Per AISC Specification J10.8.)<br />
5. On page 532, Example 15-7, in the ASD calculations <strong>for</strong> web local yielding, the<br />
comparison of Rn/Ω = 225.2 kips should be with Ca = 150 kips (not 140 kips).<br />
6. On page 533, Example 15-7, the calculation of the min t of stiffeners should include a<br />
factor of 2 in the denominator since a stiffener is located on each side of the beam web.<br />
The resulting calculated minimum thickness should be 0.179<strong>”</strong> (not 0.358<strong>”</strong>).<br />
However, the minimum thickness required <strong>by</strong> the AISC Specification must be half the<br />
flange thickness, and tf/2 = 0.605/2 = 0/303<strong>”</strong>, so the 3/8<strong>”</strong> thickness indicated is correct.<br />
Furthermore, the minimum weld size required <strong>by</strong> Table J-2.4 is based on the<br />
thickness of the thinner part, in this case the 3/8<strong>”</strong> plate, not the W12 x 87 column web<br />
thickness of 0.515<strong>”</strong>. However, the listed weld size of 3/16<strong>”</strong> is correct.<br />
Page 4 of 6
7. On page 535, Problem 15-11, in the answer, the connection is made to the column (not<br />
girder).<br />
Chapter 16<br />
1. On page 555, the notation <strong>for</strong> the lower bound moment of inertia should be Ilb (not I) <strong>for</strong><br />
AISC Commentary Equation C-I3-1.<br />
2. On page 556, Example 16-3, the notation <strong>for</strong> the factored moment <strong>for</strong> the LRFD method<br />
should be Mu = 670 ft-k (not Ma = 670 ft-k).<br />
3. On page 558, Example 16-3, under “<strong>Design</strong> of studs,<strong>”</strong> the equation <strong>for</strong> the “Total no. of<br />
connectors required<strong>”</strong> should be corrected as follows:<br />
Total number of connectors required on each side of the point of maximum moment<br />
= ∑Qn/Qn = 494/21.2 = 23.2<br />
Use 24 ¾<strong>”</strong> studs on each side of the point of maximum moment (which is C/L here).<br />
4. On page 559, Example 16-3, the concluding statement should be corrected to read “Use<br />
W18 x 46 with <strong>for</strong>ty-eight 3/4<strong>”</strong> headed studs.<strong>”</strong><br />
5. On page 565, Example 16-5, the value <strong>for</strong> the moment of inertia I used in the<br />
denominator <strong>for</strong> the calculation of ft under “stresses after concrete hardens<strong>”</strong> should be<br />
1127 (not 1129) as determined earlier in the example.<br />
Furthermore, the value <strong>for</strong> ft should be 42.93 ksi (not 42.86 ksi) and the “Total ft<strong>”</strong><br />
should be 72.83 ksi (not 72.76 ksi).<br />
Chapter 17<br />
1. On page 576, in the sixth line of the next to the last line of the paragraph beginning with<br />
the words “The original reason <strong>for</strong> limiting . . .<strong>”</strong> the notation should be Es (not Fs).<br />
2. On page 577, in the second line of Note 2, the notation should be 2.26√E/Fy (not<br />
2.26√F/Fy).<br />
3. On page 579, Example 17-1, the calculated value <strong>for</strong> Ec should be 3.2665 x 10 3 ksi (not<br />
3.410 x 10 3 ksi).<br />
Furthermore, on page 579, the calculation <strong>for</strong> Ic omits the deduction <strong>for</strong> the<br />
rein<strong>for</strong>cing steel. Thus the calculation <strong>for</strong> Ic should be shown as follows.<br />
Ic = (1/12)(20)(20) 3 – 195 – 4(1.0)(7.5) 2 = 12,913 in 4 (not 13,138 in 4 )<br />
Furthermore, on page 579, using the corrected values <strong>for</strong> Ec and Ic, the calculated<br />
value <strong>for</strong> EIeff should be 17.632 x 10 6 k-in 2 (not 18.173 x 10 6 k-in 2 ).<br />
Furthermore, on page 580, using the corrected value <strong>for</strong> EIeff, the calculated value <strong>for</strong><br />
Pe should be 8392.2 k (not 8650 k).<br />
Furthermore, on page 580, using the corrected value <strong>for</strong> Pe, the calculated value <strong>for</strong><br />
Pn should be 2137.3 k (not 2145 k).<br />
Furthermore, the value used <strong>for</strong> Pn in the subsequent LRFD and ASD calculations on<br />
page 580 should be 2137.3 kips (not 2145 kips). φPn should be 1603.0 kips (not 1608.8<br />
kips) and Pn/Ω should be 1068.6 kips (not 1072.5 kips).<br />
4. On page 581, Example 17-2, in the calculation of C3, the value used <strong>for</strong> Ac should be<br />
123.1 in 2 (not 12 x 12). Thus, the value <strong>for</strong> C3 should be 0.8903 (not 0.85).<br />
Page 5 of 6
Furthermore, on page 581, using the corrected value <strong>for</strong> C3, the calculated value <strong>for</strong><br />
EIeff should be 17.205 x 10 6 k-in 2 (not 17.026 x 10 6 k-in 2 ).<br />
Furthermore, on page 581, using the corrected value <strong>for</strong> EIeff, the calculated value <strong>for</strong><br />
Pe should be 4606.3 k (not 4558 k).<br />
Furthermore, on page 581, using the corrected value <strong>for</strong> Pe, the calculated value <strong>for</strong><br />
Pn should be 1217.3 k (approximately the value of 1217 k shown).<br />
5. On page 582, the second equation <strong>for</strong> Vn should be corrected as follows.<br />
Vn = 2√f’c b d + Vst<br />
The last term should be Vst (shear strength of the steel) not Ast (area of the steel).<br />
6. On page 586, Problem 17-7 (c), the answers should be 671 k, 448 k (not 671 k, 446 k).<br />
Chapter 18<br />
1. On page 595, the equation <strong>for</strong> Zfurnished should read as follows.<br />
Zfurnished = 2Af(h/2 + tf/2) + 2[(h/2)(tw)(h/4)]<br />
2. On page 595, the equation <strong>for</strong> Mu/φbFy should read as follows.<br />
Mu/φbFy = 2Af(h/2 + tf/2) + 2[(h/2)(tw)(h/4)]<br />
3. On page 595, in the equation <strong>for</strong> the flange area Af, the values tw shown in the<br />
denominator should be tf so that the equation reads as follows.<br />
Af = Mu/φbFy(h + tf) – twh 2 /4(h + tf)<br />
4. On page 597, when checking <strong>for</strong> compactness of the flange plates, the ratio bf/2tf should<br />
be compared with the value of 0.38 (E/Fy) ½ = 10.79.<br />
5. On page 605, the value φvVn shown in the denominator of AISC Equation G3-3 should<br />
be Vc. The value <strong>for</strong> Vc is φvVn <strong>for</strong> LRFD and Vn/Ωv <strong>for</strong> ASD.<br />
6. On page 609, Problem 18-1, a live load L = 3 k/ft (not 4 k/ft) is used in the solution <strong>by</strong> the<br />
author.<br />
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