I ’-—* ——'- "" "' «a it? A STRUCTURAL ANALYSIS OF THE ‘ MICHIGAN STATE COLLEGE LIBRARY BUILDING: II , THESIS IIIII IIII mm III B. s. i _ ' - W. B. Edwards .. “' * , 1931 :- ;. 3, ' A - — - ~~ -‘ — r ‘ _ - ‘_ _ ‘b - 2"-” ‘ PLACE IN RETURN BOX to remove this checkout from your record. TO AVOID FINES return on or before date due. DATE DUE DATE DUE DATE DUE MSU Is An Affirmative Action/Equal Opportunity Institution A Structural Analysis of The Michigan State College Library Building A Thesis Submitted to The Faculty of NICUIGAN STATE COLLEGE of AGRICULmURE AND APPLIED SCIENCE By W. B. Edwards hhula-um Candidate for the Degree of bachelor of Science June 1931 ACKNOWLEDGMENT The writer of this thesis wishes to acknowledge the assistance given him by Mr. C. L. Allen and Mr. C. L. Miller of the Civil Engineering department, also the cooperation of the Bowd-Munson Co. of Lansing, in furnishing detail plans of the steel and reinforced concrete used in the building. w. B. E. \h’ c C? 01 FL BIBLIOGRAPHY - "Roofs & Bridges" - Merriman & Jacoby "Graphic Statics" - Malcolm "Structural Theory" - Sutherland & Bowman "Theory of Structures" - Spofford "Reinforced Concrete Construction" - Hool, Vol. I & II Building Code - City of Lansing A. I. S. C. Handbook Carnegie Pocket Companion INTRODUCTION This thesis, "A Structural Analysis of the Hichigan State College Library Building", is presented as a practical problem on one phase of Civil Engineering; namely, Struc- tural Engineering. The building under consideration is located on the cam- pus of the Michigan State College opposite the Engineering Building. It was erected in 1922 by the State of Michigan; Bowd-Munson a Co. of Lansing, being the architects. The building is of brick and reinforced concrete con- struction with a slate roof supported on steel trusses. In general, the buildings may be divided into three parts: the west ell, housing the book stacks; the east ell, housing the Magazine Room, the seminars, and the College Museum; and the main part of the building in which is located the graduate study, the assigned reading room, and the main study hall. The building may also be classified, for the purpose of analysis, into the roof system, the floor system, the walls and columns, and the footings. PART I The roof system is composed of four parts, the truss- supported roofs over the east and west ells and the main sec- tion of the building and the reinforced concrete slab roof over the art gallery and main hall. The first roof to be considered is the roof over the main part of the building. It is composed of slate roofing nailed to wooden sheathing which is SUpported directly upon the purlins, 8" @ ll.25# channels, which are in turn support- ed upon the modified Fink roof trusses shown in Fig. 1 at all panel points with the exception of the end panel points just above the reactions, the roof at the end resting directly upon the wall of the building. The size of the members in the roof truss, with other data concerning the trusses is found in table 1 on the following page. The loads upon the roof trusses may be divided into two classes, the dead and the live. The dead load is composed of the weight of the truss itself supported from the panel points on the upper chord of the truss and the weights of the roof covering and purlins on the upper chord and the weight of the suspended ceiling on the lower chord which is also considered as acting at the panel points. The live load may consist of aany of several combinations of loadings acting at the panel IDOints on the upper chord, the combination producing the glusatest stress in each member being used in figuring the f1—ber stress in that particular member. These different com- biJnations of live loads are as follows: (1) snow over the en- ticre roof, (2) wind on one side and snow on the opposite side, TABLE 1 MAIN ROOF TRUSS DATA MEMBER ANGLES WT/FT. BS & B,S, 2-5x5%x5/16 17.4 CU & c,U, 2-5x5%x5/16 17.4 Dw & D,w, 2-5x5%x5/16 17.4 EY & E,Y, 2-5x5%x5/16 17.4 SR & 3,3, 2-4x5 x5/15 14.4 TQ & T,Q, 2-4x5x5/18 14.4 VP & V,P, 2-4x5x5/16 14.4 20 a 2,0, 2-4x5x5/18 14.4 ST & s,T, 1-2%X2x% 5.62 TU & T,U, 2-2%x2x% 7.24 UV & U,v, 2-2%x2x% 7.24 vx & v,x, 2-2%x2x% 7.24 xw & x,w, 2-2%X2x% 7.24 WY & v,y, 2-2%x2x% 7.24 xz a X,z, 2-2%x2%x% 8.2 YZ a Y'Z, 2-2%z?%x% 8.2 zz, 1-2%X2x% 3.62 Total weight 2374# LENGTH VI 7c 7t 71 4I 4t 9! 5r 4r 5! 91 10' 91 51 gr gr 17' AREA (in2) 5.12 5.12 5.12 5.12 4.18 4.18 4.18- 4.18 1.05 7.24 2.12 2.12 2.12 2.12 2.38 2.58 1.06 and (3) wind on one side and ice over the whole roof. The dead load on the main truss is computed as follows: the total weight of the truss itself as taken from table 1 is 2474 pounds, which, when distributed equally over the upper chord, produces a load of 264 pounds at each of the inter- mediate panel points and 152 pounds at each of the end panel points; the weight of the roof covering is equal to the area of the roof supported by the truss times the weight of a unit area of the roof, the area being 586 square foot per side per truss, and the weight being 11.25 pounds per square foot and the sheathing 4.00. This makes the total weight of the roof covering 4542.5 pounds, which, when divided equally among the panels, produces a load of 960 pounds at each of the in- termediate panel points, and a load of 480 pounds acting dir- ectly upon the wall at each end. The dead load caused by the purlins at each panel point is obtained by multiplying the distance between trusses (13 feet) by the weight per foot of the purlins (11.5 pounds) and is equal to 150 pounds per panel point. The weight of the suspended ceiling on the lower chord is taken as 10 pounds per square foot producing a load of 130 pounds per foot upon the chord of the truss. This is divided proportionately amoung the various panels as is shown in the load schedule in table 2. In considering the live load, the snow load is taken as 10 pounds per square footl, and the ice load is taken as the same, While the wind load is considered as being 20 pounds 1. "Theory of Structures" - Spofford per square foot on vertical surface2 and the component nor- mal to the surface is figured. by the formula Pu = R! 2%; . These live loads are also shown in tabular form in table 2. All stresses in the members of the main truss were found by graphical methods, the stress in the ambiguous mem- .bers wx and w,x, being found by the method as described in Art. 25 of Part II of "Roofs & Bridges" by Merriman a Jacoby. These stresses are found in table 5, and the graphic solutions are found in Figs. 2, 3, and 4. The Fink roof truss which is used on the east ell is shown in Fig. 5 and the size of the members is shown in table 4. The method of computing the loads on the truss being the same as that used on the main truss, the distance between trusses being 16.53 feet, and the roof area per truss being 405 square feet. The loads on the east e11 trusses are shown in table 5 and the stresses are shown in table 6 with the graphical solutions in Figs. 6, 7, 8, and 9. The third part of the roof system, the roof over the west ell, is somewhat different than the others in that the truss used to support the roof is statically indeterminate under unsymmetrical loading such as snow 6r wind on one side. This makes necessary certain assumptions in the computation of the stresses, these assumptions being explained in the discussion of the computation of the stresses produced by the unsymmetrical loading. The data regarding the members of this truss is found in ‘ 2. Building Code - City of Lansing. T' NOTE SINCE Tzuss as SYMMETRICAL ABOUT : ONLY ONE HALF is SHO\VN ' ,1 t} ' W‘9«.l ‘ V s_ili MAIN TEUSS‘ ICE ON \VHOLE IZGDF' SCALE l”= looo" i .009... quom “t WMDNE. 27:2 20 DZ.) U Nana > ukok ‘3 grown — w 3 / .u 3) :0...T=¢\. widow 4.5 FWQM IWWDNC. mafia... I a o 2 S. N > w x > 3 F u >/ o m \V (><>< EAST ELL - DEAD LOAD SCALE I"=Iooo* I”) ab “:‘L / 2P t EAST EL. L- ICE ON \VHO SCALE (2500’ LE POOP \V-l / uy; K- P t S TEESS DIAGIZ AM E. PEACTIONS EAST ELL- \VIND ON LEFT SCALE I”: :000“ \V a-d 7:1 e uy K‘F z-t f gm EAST ELL - SNOW ON EIGHT SCALE - 11500“ TABLE 2 LOADS ON MAIN TRUSS LOAD DEAD SNOW 0R ICE WIND AB 150 BC 1580 970 1550 CD , 1380 970 1550 DE . 1:590 970 1550 EE' 1580 9V0 775 E'D' 1580 970 D'C' 1580 970 C'B' 1580 970 B'A' 130 AR 500 HQ 600 QP 900 P0 990 00' 780 O'P' 990 P'Q' 900 Q'R' 600 R'A' 300 Left Reaction 8140 5595 5050 Right Reaction 8140 3595 2400 Note:- All loads vertical except wind which is normal to the roof surface TABLE 5 STRESSES IN MAIN TRUSS NENBEFS .MEMBER DEAD ICE 0N WIND MAX. ' STRESS WHOLE ROOF . BS 15550 C 5900 C 4460 25690 CU 11940 C 5550 C '4460 21750 DW 10120 C 4750 C 4460 C 19550 EY 9550 C 4160 C 4460 C 17950 R3 10820 T 4850 T 5200 T 20870 QT 10640 T 4850 T 5200 T 20690 PV 9050 T 4140 T 5850 T 17040 OZ 6120 T 2750 T 1170 T 10040 ST 640 T 0 0 640 TU 1470 C 810 C 1550 C 5850 UV 2210 T 700 T 1520 T 4250 VX 2970 C 1590 C 1550 C 6110 XW 960 T 710 T 1520 T 2990 WY 1150 C 810 C 1550 C 5510 YZ 4580 T 2050 T 5950 T 10560 X2 5580 T 1540 T 2590 7510 ZZ' 780 T 0 0 780 X'Z' 5580 T 1540 T 0 4920 Y'Z' 4580 T 2050 T 0 6610 WVY' 1150 C 810 C 0 1960 X'W' 960 T 710 T 0 1670 V'X' 2970 C 1590 C 0 4560 HOP-3665380000 O 801-] oeeea MEHBER U'V' T'U' SIT! oiz: P'V' tht R'S' E'Y' thv C'U' BIS! TABLE DEAD STRESS 2210 1470 640 6120 9050 10640 10820 9550 10120 11940 B *3 v3 0 c: C) .3 a (cont) ICE 0N WHOLE ROOF 700 810 0 2750 4140 4850 T C 000081—3813 VII N D 0 0 0 1170 1170 1170 1170 5500 5500 500 5500 r—3 0 O C) 9—3 3-3 *3 0 MAX. 2910 2280 640 10040 14560 16660 16840 16790 18170 20570 22550 Maximum Compressive Stress is 4640 pounds per square Maximum Tensile Stress is 5000 pounds per square (DP—3 1-3 00005353538 inch inch MEMBER BQ & CS DT QK 2° 8° 2° 2° C: L?” h—‘D 93 ST 311 U) R°R° 898° TU Y0 ‘ YN YZ YX XW TABLE 4 EAST ELL TRUSS DATA ANGLES 2-4x5x5/16 2-4x5x5/16 2-4x5x5/16 2-5x5x5/8 2-5x5x5/8 Total weight WT/FT 14.4 14.4 14.4 25.0 25.0 25.0 5.62 7.24 7.24 8.2 7.24 1200# LENGTH 7' 11%" 7' 11%" 7' 114" 5' 8%" 5' 8%" 5' 7-5/16" 4' 5-5/16" 6' 6" 8' 10-5/8" 15' 6-9/16" 14' 6" AREA (ing) 4.18 4.18 4.18 6.72 6.72 6.72 1.06 2.12 2.12 2.58 1.06 TABLE 5 LOADS 0N EAST ELL LOAD DEAD SNOW 0R ICE SNOW 0N RIGHT WIND AB 100 BC 1150 675 1550 CD 1150 \ 675 1550 DE 1150 675 558 675 EF 1150 675 675 RC 1150 675 675 GR 100 AK 470 KL 940 LM 940 MN 940 N0 940 OF 940 PH 470 Left React. 5795 1688 506.5 1540 Right React. 5795 1688 1181.5 1850 Note: - All loads vertical except wind which is normal to the roof surface. TABLE 6 STRESSES IN EAST ELL TRUSS MEMBERS MEMBER DEAD SNOW ICE ON WIND MAX. STRESS ON RT. WHOLE 0N LEFT BH 9590 C 925 C 5110 C 2250 C 14750 C CS 7450 C 925 C 2490 C 1850 C 11770 C DT 7450 C 925 C 2490 C 5150 C 15090 C KQ 6700 T 670 T 2260 T 2840 T 11800 T LR 6700 T 670 T 2260 T 2840 T 11800 T MU 5650 T 585 T 1200 T 500 T 4150 T QR 940 T 0 0 0 940 T RS 1550 C 0 500 C 1400 C 5450 C ST 1150 C O 675 C 1900 C 5725 C TU 4560 T 150 T 1550 T 5590 T 9500 T UV 940 T 0 0 0 940 T VW 4560 T 1500 T 1550 T 200 T 6510 T WX 1150 C 675 C 675 C 0 1825 0 XY 1550 C 500 C 500 C 0 2050 C YZ 940 T O O 0 940 T NV 5650 T 585 T 1200 T 500 T 5150 T CY 6700 T 1525 T 2260 T 580 T 9540 T P2 6700 T 1525 T 2260 T 580 T 9540 T EW 7450 C 1500 C 2490 C 2190 C 12150 C F1 7450 C 1500 C 2490 C 2190 C 12150 C 02 9590 C 2125 C 5110 C 2190 C 14690 C is 5550 pounds/sq. inch Maximum compressive stress 1750 pounds/sq. inch Maximum tensile stress is A. . "l. ‘ .I I ‘ .15 50>, - 353 L8» table 7 and the loads on the truss are found in table 8. The dead stress in the members of the truss have been computed by the method of joints, these computations being shown in the following paragraphs. 5898.5 St ess - _ r 5 r (BR) .70., 559095 c 95 H t 898 5# S e S :3) o A I" 8 (AH) T . 3995 EM: 0 5898.5(9.91) - 1559.4 (4.95) - 7.01 8(CNT 0 ’5“ s - 44004‘ c 6 (CK) A, R _ I: 5 1559-4 (-.90) 7.01 3(HK) o H 3(HK)= 1100# c 13900 A530 2M=0 = # S(KN) 779.7 T -——i 3900 MENBER BH & GS CK & FP DM 5 EM HK & PS KN & NP MN HNS-A TABL 7 L13 WEST ELL TRUSS DATA ANGLES 2 - 4x5x5/16 2 - 4x5x5/16 2 - 4x5x5/16 2 - 5x5x5/16 2 - 5x5x5/16 2 - 5x5x5/16 18" - 20" G Total weight wr./FT. 14.4 14.4 14.4 12.2 12.2 2.2 *- 1159.41# LENGTH 71- 7:- 7!- 7t- 91- 9!- 291- 1/8" 1/8" 1/8" 1/8" 11" ll" 9" * Weight of Girder beam considered elsewhere AREA (ind) 4.18 4.18 4.18 5.56 5.56 5.56 TABLE 8 LOADS ON WEST ELL LOAD DEAD SNOW 0R ICE SNOW 0N RT. WIND BC 1560 1080 2160 CD 1560 1080 2160 DE 1560 1080 540 1080 EF 1560 1080 1080 F0 1560 1080 1080 GA 95 AB 95 Left Reaction 5995 2700 810 V 1550 H 1915 Right Reaction 5995 2700 1890 V 5825 . H 1915 Note:- All loads vertical except wind which is normal to the roof surface. 2M=0 c 1559.4 (9.91+4.95) = 9.915 s 7 K N # (ILN) ” §Fv=o f A S(DM)==5898.5 - 2(1559.4) €‘.707'= 110d# 0 K ._ , .. g # The stresses in the members on the opposite side of the truss are the same as those already computed. The stresses for ice or snow over the entire roof are shown in Fig. 11 and are included in the table on stresses in West ell members, Table 9. From this point on the truss becomes statically indeter- minate if the entire truss is considered as a unit with reac- tions at each end of the supporting girder beam, but if the Upper portion of the truss is considered as being SUpported by the girder beam with reactions at the four points where the truss is fastened to the girder H, N, S, A, the stresses for conditions of unsymmetrical loading may be readily computed. Following is the solution for snow on the right side of the truss. The loads as given in Table 8 are DE =540#, EF & FG== 1080#. These loads are considered as being transmitted to /:\ 3 \VEST ELL- ICE ON \VHOLE IZCQDF‘ SCALE- \”= 1000‘ the beam along the most direct route causing reactions on the beam, reading from left to right, of 0, 270, 1890, and 540 pounds, respectively. With this assumption the stresses may be readily figured by the method of joints. Since the left reaction is zero, it is apparent that the stress in members BH, HA, HK, and CK must also be zero. =540 -.‘- .707 =750# c S # =7 .70 '-'-‘ , A [080 J40 F S 1080 760# p G (PS) ‘ .707 X '5' C 5 6'40 0 E S 540 - 580 M (DM) I 2(,'70'7) C SUN?) = 540 =380# C s = 270*" (KM) C 3(MN)==580 X .707 = 270# T =(3 S(CK) . mo E # S = 3» + . , = 3, M ,F (NP) 1030 707 x580 1 50 C N’ ‘p Considering the reactions as concentrated loads upon the beam, the reactions upon the walls may be determined by the equation 2M: 0. (270)1 + (1890)2 + (540)5 = 5 R (right) a # R