m .;T——— m "Wm”! A DuifiN..Cfl[cx 0le . . :ocom‘oc .Dscx mm: 1 mama 383.96! ”CHOAN "A," CCU-80.3 a» 1x .' xx 3,. . . 1"- ‘o-V I '3 ‘1‘, "51' 1 my; _ " " ‘ 3 ‘ . .-‘ . U‘. . ‘.y I .3» ”A?“ A}. , o; ’3‘ J (1:2 I ,\ -‘ '_ ”:65.!’~T;% i v '. , “a S f 5 fi.‘ ‘y } .2 t 7, ._,_H..j “3”; g '2: - - is" I $ ‘ ‘ a’- ‘ 3 ’3.qu ‘ {£35- v ;_; ‘3‘. ‘. 4 5 J“- y . 1: “Li" 3; ‘ .‘1 ‘ _ ‘- 1‘ .tfi.l..'r,_. JI-‘mfrgyhu - .‘ V '13”. C r. 4 l 't’.v 1. . -.‘ .J . w,_ "L V .._. ,. -. ‘. u I ' \-’ 'I-l“ g}, , ‘s.|,l\ a 4 \- u ‘39.: km- ,".n . . :,L/._ _ an}? '~ . ‘ ' ‘ ‘1‘ . ”'1‘. . A in 3‘ {1* .~‘_ g k ‘ "a .. - w’ ‘ '1...) 1' ,, _ _ g." 'WA'N‘ . >."‘ B- '9' . " '17-! "‘2. )9“ .‘ ..';y-\.z- -_ - _ ;-. 'gri-:.\'I,l"' * '. a I . _.‘.AJ . . .\‘ '15. , ’ L. . ‘5} :‘.'¢ ‘. - l%.,~v::."; ‘1‘ A ' ,i‘ 1-": 4... .- . v, '19, (-5 — 0 .' .L I“. 4 IO'.-. ‘ '. ‘u'.‘.j' .. . , D'r. - “ A .— h, . ,w'egt’ ~ ’$-$' 'v( th‘ ‘< V -..:a‘i.ft:_“‘¥ :’ ’1‘"; ; amt-f? Kw ’ . ' 2‘ “('4 ‘. !~'. " "fluff”? ‘ ‘3 4 " I; y”.‘ ' w‘.—*‘~r‘r€;_-~ 5634' g ‘4 ' "Whig“? - ~ ‘.";3:":)F"." -.-.§i:,' ." " .I . ' - 't,‘w'}tfi;(‘; "pf . 6"”! .' (J's ‘ "‘ ' . wrigw.‘ " ‘ — ." I. k.‘ .‘. V . 1.."V/Tl."l ~. 'T'.I"'73£I"‘: '- :‘t J x‘ & ' u ‘1, f 1.4““, ' '.' ‘51- ' > lls 1'. \ ‘ _ if. ’ a”; .1 :0 3"- " f'.‘ \ .fl _¥ ‘ f ’ : h i .1 ... . .4 -’ "l.‘ u‘ ' " ‘. '0 D . \ ,_ ' .' _‘ -. .-. ‘I‘ ‘ K "‘ ' ‘ W l s. _ - V‘I . I‘. v. V} _. '_ . . “A; J3..- _ . .Ik. ' ‘ .I "J! '1- - I . I. I._'- '.‘ ‘74 ”-~ ' . ,, _ J -~‘ ‘ _ . '4 ‘1‘ "\I a‘. ‘t( o ' _ - D . ' f 'n“ q, ' I ‘v. ‘Q‘ I . .‘Z x i I ‘ kl ,‘I . ‘. f \ " H” -. r M'.’ .' r '1 ' ' ' ' " ‘ .fi". ‘fifi " "If {If - S A ‘ . :3 { TA"; .4): ufi$x ,x . 2'}: . ' z L ‘ "4m - ,; .".; fl‘ '. A‘ u . " ‘. "' 1 I. ' I’ I I ‘N r- . . I' l. . ‘ " ' . ‘ ‘ ‘ .' y. . . “ '. "t; V ' ' EU I n n . ‘9“| I ‘ t . . k“, , "it. ~ 33 ‘9‘» ' .' a . .2 r. (3 ‘K ' ‘. "s V. 1.. f”; “a: .‘13‘ ’.., . .n.\l-.(".“'I “13K: ‘Wfifi‘ A Design Check Of The Ocqueoc Deck Truss Highway Bridge A Thesis Submitted to The Faculty of MICHIGAN STATE COLLEGE of AGRICULTURE AND APPLIED SCIENCE by F. M. Drilling M Candidate for the Degree of Bachelor of Science June 1941 THE” INTRODUCTION This thesis is a partial design check of the design of a deck truss highway bridge which was designed and built by the Michigan.State Highway Department. The bridge is located in Presque Isle county in northern Michigan. It spans the Ocqueoc River at station 8032 I 18 on highway'US 23 and is found in Ocqueoc Township about sixteen miles northwest of Rogers City. The span of the structure is one hundred feet, and its total width is about forty feet. It is equipped with side- walks and standard railings on each side of the reinforced iconcrete roadway. The specifications used in the design were the Michigan State Highway Department Specifications for Bridge Design of 1926, but the design was checked using the revised edition of these specifications which was adopted in 1936. The structure was designated as a Class A bridge and was therefore designed for standard H-lS loading. It was the object of this thesis to give the author some practical experience in the checking of a design of this type and to better acquaint both the readers and the author with the‘ methods and prodecure used in the design of a highway bridge. As it was impossible to cover the complete design in the time allotted, only the superstructure was checked, and the abutt- ments and some of the details were not touched upon. In conclusion, the author wishes to acknowledge his special appreciation to MI. W. A. Voigt, Bridge Design Engineer of the Michigan State Highway Department, for his kind help in the securing of the plans and specifications necessary for this -1- 138349 IIx‘TRODUC'l‘IOI‘I (con' t ) project, and to the faculty members of the Civil Engineering Department of Michigan State College, for their cooperation and aid in problems involving the technical points of design. ’ ~ 00 .00\ .me \\ .QNNNN u. wcxxx as k magma .mo ZOHBSVHAQ WEIGHT OF SLAB (2 ”Crown . l + 3, 00 I a; .-%:: I: L___m L, :m9’.z" .J VII ’1 AREA OF SLAB Rectangular Part (8/12)(38 l/éi- 25.45 Sq. ft. Use the crown as triangular (2/12)(38 l/6)(l/2)= 3.18 sq. ft. Small rectangles at end under slab §12§6 §[8§{2)- 0.09 sq. ft. 144 Total- 28.72 sq. ft. Use 28.8 sq. ft. WEIGHT PER FOOT OF SLAB Use w: l50#/cu. ft. (28.8)(l)(150): 4320 # per foot WEIGHT OF SLAB APPLIED TO EACH TRUSS £3239: 2,160# per foot 2 WEIGHT OF SIDEWALKS AND RAILINGS £936 AREA OF CAL LALK (52.5)(1o)-(s)(;)- 2.43 Sq. ft. \:‘1 ' V.“ ‘V y€f\ ' . 1 x.- it ,1-‘.. fi‘.‘ n « x. -7 :‘aA A‘ .LJ‘IhlJ A. J Lind—a. J.‘ 1.2le vn‘ w‘vm v," ‘-x r'1 ‘\ V; :1 " -"' u~;“ 'j 35f“'r‘ .“7_."";,'.' “v- "I‘Jfll 1);...1. i‘COl UP “no. 1.1). Di‘himflum i‘JilLluu n1}; Linn) IL in; W: 44#/ft- l.‘.-‘_r"-1 ,o‘r‘ «'Y‘r‘u’" TOTAL W“IGhT CF RAILIXG ancilCLS HUT IuoLLJIJG GhCnhim WEIGEI CF SCAG RTE dAILInG POSTS WEIGHT OF ONE IUTEEMZDIATE PLST q I ‘ I» I ’3 A (3 l/3)(i 1/3)(1 9/:4)= 5.4 cu. 1L. (5 [‘(IFO)- “‘flfi JO 1*) J 0-1-th Applied at each intermediate panel truss. <3 2/3)(2 5/24)(1 5 2:): 9.: cu. (9.8)(159)- 147C? EACn TRLSS ”1:"..fim i‘sJJJ. point on each An lied at each end panel point on each truss WE IGIIT OF STRIDIGERS A/c/k h/a M 5/06 1,7,1 191% i l- k; /2 X5] 3.6’# I l TOTAL WEIGHT PER FOOT OF STHIJGERS (9)(35)= 315# per foot. WEIGHT PER FOOT OF STRINGERS TRANSFERRED TO EACH TRUSS élfia 158# per foot. 2 WEIGHT OF STRINGERS TRAI'ISFEPRED TO EACH TRUSS AT EACH II‘JTERW‘DIATE PANEL POINT (11.104)(158): 1,755# WEIGHT APPLIED AT EACH END PAE‘IEL POINT 172'5: 878# 2 WEIGHT OF LCOR BEATS F. .37“'.3” ._.. :1: :_: z: z: z: z: z: [ .5 .4 " .z”z”’;’J 32 X35 If “/0 14»ng .. 7» In , .Aflzg"¢a72f [abfib fm- end floor My: WEIGHT OF END FLOOR BEAMS /2[ '2 ”’27:; 10/07: 7Gw- nmfiwvnemfiaflr érnams Size-—24" x 12" x llO# Weight of Concrete: (2)(l)(38)(150)= ll,400# Weight of RI Beam— (llC)(37.67): 4,150# Weight of 2 plates: (2)(35.7)(27.5)= 164# (12 ’ @ 35.7#/ft. Weight of 18 Hitch Angles 3% x 3% x é-lC" @ ll.l#/ft.- (18)(ll.l)(1o)=_ (l) 2 167# Weight of 162 Rivet Heads @ 21#/lOO. (2l)(l.62)= 34# Total= 15,915# Io .. I L fl Garret g ‘0 N \\\\t________i_lL_ fad Hoar“ 49mm Weight of end floor beam applied to each truss 1i,315 a 7,958# WEIGHT OF INTE.TEDIATE FLOOR stems Size 24" x 12" x lOO# Weight of RI Beam: (lOG)(37.67): 3,767# Weight of 2 plates: (2)(30.6)(27.5); 141# 12 Weight of 36 Hitch Angles 3e“— x 3-i- x - 10 9 11.1#/rt.= (36)(11.1)(lg); 3339! (1.2) Weight of 216 Rivet needs. @ 21#/lOO- (21)(2.lo): é§# -7- WEIGHT OF INTERUEDIATE FLOOR BEAMS (con't) Total: 4,287# Weight of Intermediate Beam applied to each truss at each panel point. 428 7 2 2 ’ 144/1” 2 YEIGET OF EXPANSION ANGLES WEIGHT OF ONE EXPANSION ANGLE-~E A 2 (2)(1.4% 1.5) x 33': 39' of angle 39' of 3%x3 x 3/Sze 7.9#/ft.: 308# (2)(2'8"/ 10") g 33': 40' of plate 40' of 8" x B/L" plate O 20.4#/ft.. 816# Total: Sle/ 3tS: 1124# WEIGHT OF ONE EXPAGSIOG AEGIE--E A 2 (2)(2'8"/ 1'4")/ 33'- Al' of angle 41' of 3; x 3 x 3/8"£@ 7.9#/ft.- 3245! (2)(2'8"/ 10") / 33’- AC' of rod 40' of B/Z" Square rod @ l.9lB#/ft.= 77# Total: 324 z 77: 401" TOTAL WEIGHT OF EXPANSION ANGLES APPLIED TO EACH TRUSS AT EACH END PANE POINT 1124é 401 - 703# WEIGHT OF LATERAL BRACING TOP CHORD .9 . , ‘-L”- n n n 7/5- l0.0.f «_20 M53' 30’ l /4' r 14¢45’ if AR 3 RR 7aumw 7' NAM/(1w! luv: 3‘3: Srkess I~ o at 3- Load ed Length- 11.135 A (4)(11. 1-14) A (5/9)(u .104): 99.5 ft. LIVE LOAD STRESS IN "L" TNT TO TSVOV TRAIN LOATIVO RS: (30.15)§11.53) A (10.05)§41.55) A (40.?0)(55.55) 100 . . .)_ .- .'. (10.956) 3&0 IIPACT STRESS (19. 54 9(49.7)_ 9.3 kins SIDEVALK AND FAIIIHG IIVE T.CAU SIR? SS ES P(Sidewalk)- (40 A 3099) (55— 3/3): (SS)(IT w(railing)= 100#/ft. w(total)- (93.9)(5/3) A 100: 256#/ft. as RR: (.2561(99.5)(92.5 : 5.0 kips ‘ €100) L f: (.D. 39)g9.941(e.94) 0.9 kip 11.1047“T:7": gr O ‘70- 5-0 - 0.5- 4-4 so: (4-4H 5';OO>- 6.2 kips (10.358 TOTAL IIVE LOAD AN D II'PACT ST FE SS IN "TNDSS "0" 19"" 42.7 A 9.3 A 9.2 - 37.2 kips tension LIAXIEJTUJ LIVE LOAD AND IMPACT STRESS-ES IN FET'BL“S "P" AITD "R" 34/! mar «ya 20 753" 3 .1! l1' 1 0.1:” 1453’ 30' /4' I.» jkfl l (R M IIIIIIIII"‘--LL_§~f3:zz:j:i:2””’,,,LA’~"”IIIIIV fawn/an: Luvs .. fix! 512:3: In P 7?» non IVFZt/EIVCE [ave Rx STRESS 7N ”I? a LIVE LOAD STRESS IN "P" DUE TO TRUCK TRAIN LOADING RR: 130.121111.5§) A (10.05)(41.55) A (40.20)(55.55);A7 _71P 239' l f7:i1 £17.55)(85.55) ALI3o.I5)(99.55) , 1 100 ad . k RR: 66. 5 kips 47"” 66¢r' 2£Mo= 0 (66.5)(44.45)= (30.15)\44)A (7.55)(30) A (Sp)(lo.958) Sp--128.0 kips IMPACT STRESS (19.35%)(128.0)= 24.8 kips SIDEWALK AND RAILING LIVE LOAD STRESSES RR: 11.3 kips time: 0 (Sp)(lO.958) A (7.2)(22.22)g(10.1)(44.45) 2.1 24 24 1.2, fl: 1.2 klps Sp: 26.4 kips +13 T 2 4 P aA' TOTAL LIVE LOAD AND IMPACT STRESS IN IviElu-IBER "P" ”,3 128.0 A 24.8 A 26.4= 179.2 kips compression TOTAL LIVE LOAD AND IMPACT STRESS IN MEMBER "R" 1732‘ If ZFh: 0 Sr: 179.2 kips tension €7I MAXIMUM LIVE LOAD AND IMPACT SIRESSES IN MEMBER "Q" ‘3 J5’ azaS‘ 4&120 4453'S1 .30’ /4’ r vjxcr’ 7 0 LR 3 3W“ i3- .JKQszuamme lums' Fig Sfiwess .17: “(9 p Loaded length 62.5' LIVE LOAD STRESS IN "Q" DUE T TIUCK TRAIN LOADING RR- 30.0 kips ‘ ' I 23,. 0 A? / Sq- 30.0 kips IMPACT STRESS (19.35%)(30): 5.8 kips 30‘) SIDEWALK AND RAILING LIVE LOAD STRESSES IN "Q" P(Sidewalk)- 93o9#/€q. ft. w(railing)= lOO#/ft. W(total)- 256#/i‘t. f: 0.6 kip ) I6 RR: 5.0 kips l//i;;;/' 2£Fv= 0 Sq: 5.0 - 0.6 /, k s = 4.4 kips ‘52 q TOTAL LIVE LOAD AND IMPACT STRESS IN "Q" 30.0 A 5.8 A 4.4: 40.2 kips compression MAXIMUM LIVE LOAD AND IMPACT STRESSES IN MEMBER "S" (illustration con't on next page) -37- 4“ ~30' /1’ v .53253" 5 1R 77.03/01! NR J7wuu5~t£ luv: 54 STRESS I” "5 .. Loaded Length- 100/2: 50' LIVE LOAD STRESS DUE TO TRUCK TRAIN LOADING RR: £30.15)(0.45) X (10.05JI30.45) % (40.20ll44-45): 21-1 kips 100 (— 1a,: 0 vs: 21.1 (10.958) IMPACT STRESS (19.35%)(30.1)= 5.8 kips 21/ SIDEWALK AND RAILINC LIVE LOAD STRESSES IN "S" P(sidewalk): (40 / 3000)(§§‘- 5/3): 107#/sq. ft. (50) (50) Use P: lOO#/Sq. ft. w(railing): 100#/ft. w(total): (100)(5/3) / 100= 267#/ft. <24 2; RR. (.267 0)(25)= 3.4 kips ‘5 (100 f: (.267)(ll.10 )(l/L): 0.4 kips 2 M 2}}; 0 V3: 3.4 - 0.4: 3.0 SS: (3.0)(15.600): 5.3 kips (10.958) TOTAL LIVE“. LOAD AND IMPACT STRESSES IN LENDER "S" 30.1 / 5.8 / 4.3: 40.2 kips tension or compression Since a reversal of stress takes place in one passage of the load, the design stress must be increased by 50%. (con't) (con't) (150%)(40.2)= 60.3 kips tension or compression MAXIMUM LIVE LOAD AND IMPACT STRESSES IN MEMBER "T" Ajr£r. 2H3. .¢aza [405* ./5' 0.4 . ' l I /” l M 30 r A 30 3 11.55' ‘4 ARR W I'M-(valves 1m: Fin! Snug-“$5 IN 7' " LIVE LOAD STRESS IN MEMBER "T" DUE TO TRUCK TRAIN LOADING RR: 130.15)10.45) £_17.55)(14.45) {'140.20)(44.45) z 100 (10.051158.45) { (30.12)I88.45) "°5’ saxs' 100 *g/‘Y 0 l 30 l RR: 51.6 kips €// <4 c , {MO-.- 0 $5155 (51.6)(55.55)= (St)(10.958) / (10.05)(14) ,1 (30.15)(44) 576 St: 127.4 kips IMPACT STRESS (19.35%)(127.4)= 24.7 kips SIDEWALK AND RAILING LIVE LOAD STRESSES IN "T" 2‘7 .4 . . “3 BIL-.- 11.3 kips +7.7— 2 "7 2f f : 2.4 kips l I: . ) k f2: 1.2 klpS 21110: O //.3 (10.1)(55.55):(St)(10.958) / (9.6)(27.76) St: 26.9 kips TOTAL LIVE LOAD AND IMPACT STRESS IN MEMBER "T" 127.4 / 24.7 / 26.9: 179.0 kips compression -39- '11 P1 C? O MH‘IQ 4 r1. -40- TOTAL STPESSISS I}? TRUSS 1~ 7.332.] S I}? IiiII-‘S ‘EI'I BIND OF DEAD LOAD LI’TTJ LOAD TOTAL STRESS S‘IILLSS 87123338 ARIA; 1- ' ' .SIIOLS Compression 196.9 98.0 294.9 None 0 .0 O . 0 0 .0 Tension 240.7 115.6 556.5 Compression 171.5 82.4 255.9 Compression 165.5 81.0 246.5 Tension 171.5_ 2.4 255.9 Tension 180.5 95.1 275.4 Compression 299.9 157.8 457.7 Compression 125.1 66.8 189.9 Tension 299.9 157.8 457.7 Tension 120.2 75.9 196.1 Compression 585.5 169.0 554.5 Compression 80.9 55.5 154.2 'Tension 585.5 169.0 554.5 TenSion 50.1 57.2 117.5 Compression 428.5 179.2 607.5 Compression 58.7 40.2 78.9 Tension 428.5 179.2 607.5 Tension or Compression 0.0 60.5 60.5 Compression 428.5 179.0 607.5 UNIT STRESSES IN LOWER CHORD MEMBERS IN OUTER THREE PANELS (Members "B", "F", and "J") NET AREA OF SECTION 2 plates 18" x i" - (2)(1)(%)= 16.00sq. in. 4 angles 6 x 4 x 7/16 - (1)£Z%= 14.97Sq. in. (16 TOTAL: 30.97sq.in. ALLOWABLE STRESS IN TENSION: 18,000#/sq. in TOTAL STRESSES IN MEMBERS "B", "F", AND "J" Member B: 0.0 Member F- 253,900# tension Member J: 437,700# tension MAXIMUM UNIT STRESS IN MEMBER "B" S- 000 : Ono #/Sqo in. 30.97 MAXIMUM UNIT STRESS IN MEMBER "F" SF: 255'320 e 8.200#/sq. in tension MAXIMUM UNIT STRESS IN MEMBER "J" SJ: 433,330- 14,150#/Sq. in. tension UNIT STRESSES IN LOWER CHORD MEMBERS IN MIDDLE THREE PANE (Members "N" and "R") NET AREA OF SECTION 2 plates 18" x 5" - (2)(l)(%)= 16.00 sq. in. 4 angles 6 x 4 x 3/4 - (l)(3/4)= 24:26 sq. in. TOTAL: 40.76 sq. in. ALLOWABLE STRESS IN TENSION= 18,000#/sq. in. TOTAL STRESSES IN MEMBERS "N" AND "R" Member "N" : 554,500# tension Member "R": 607,500# tension -41- MAXIMUM UNIT STRESS IN MEMBER "N" Sn: 555,500 : 13,600#/sq. in. tension 40.76 MAXIMUM UNIT STZESS IN MEMBER "R" Sr: 607,500 = 14,900#/sq. in. tension 40.76 UNIT STRESSES IN DIACONAL MEMBERS IN OUTER TNO PANELS (Members "0" and "0") NET AREA OF SECTION FOR MEMBER "C" 1 plate 11" x 5/8" - (2)(1)(5/8): 5.63 sq. in. z. angles 5%: 32;" x 3/4" - (DO/4): 20.24 sq. in. TOTAL= 25.87 sq. in. ALLOWABLE STRESS IN TENSION= 18,000#/Sq. in. TOTAL STRESSES IN MEMBERS "C" AND "G" Member "0": 356,300# tension Member "G": 275,400# tension MAXIMUM UNIT STRESS IN MEMBER "C" Sc- 326,300= 13,800#/sq. in. tension 25.87 MAXIMUM UNIT STRESS IN MEMBER "G" sge 2;g,§20 : 13,700#/sq. in. tension UNIT STRESSES IN DIAGONAL MEMBERS IN CENTER FIVE PANELS (Members "K", "O", and "8") NET AREA OF SECTION 1 PLATE 11" x 3/8" - (2)(1)(3/8)= 3.38 sq. in. 4 angles 5" x 3%" x 3/8" - (1)(3/8): 10.68 sq. in. TOTAL= 14.06 sq. in. -42- ALLOWABLE STRESS IN TENSION: 18,000#/sq. in. TOTAL STRESSES IN MEMBBP Member "K": 196,100# tension Member "0": 117,300# tension Member "S": 60,300# tension AAXIMUM UNIT STRESS IN MEMBER "K" 8k: 132,520: l4,000#/sq. in. tension MAXIMUM UNIT STRESS IN MEMBER "0" So- 1171§00 : 8,350#/sq. in. tension 14.06 MAXIMUM UNIT STRESS IN MEMBER "S" SS: 60,320: 4,290#/sq. in. tension UNIT STRESSES IN UPPER CHORD MEMBERS IN OUTER THREE PANELS (Members "D", "H", and "1") _4» GROSS AREA OF SECTION CT." _ +[_ 2 plates 18" x e". 18.00 sq. in. 4 angles 6" x 4" x 5/8": 23.44 sq. in. TS " TOTAL: 41.44 sq. in. [ MOMENT 0F INERTIA OF SECTION , IX--2 plates: (2)(l/12)(§)(183)= 486 in4 4 angles: (4) 21.1 / (5.86)(9.25 — 2.03)2 = 1306 in!“ Total Ix: 1792 in.4 Tye—2 plates: <2)(18)(s3) ; (18.00)(6.502)=765 in.4 4 angles: (4) 7.5 % (5.86)(6.75 / 1.03)2 - 1447 in.4 Total 1y: 2212 in.4 LEAST RADIUS OF GYRATION OF SECTION rIyE7X .TTTQZA - 6.56" UNSUPPORTED LENGTH OF MEMBEIO -43- L: (11.1)(12)- 133" ALLOWABLE STRESS IN COMPRESSION FOR MEMBERS "D", "E", AND "L" L/r: 133 : 20.3 SC- 15,000 — l/4(L/r)2 : 15,000 — (l/4)(20.°2) 6.56 SC; l4,897#/sq. in. TOTAL STRESSES IN MEMBERS Member "D": 253,900# compression Member "R": 437,700# compression Member "LR: 554,500# compression MAXIMUM UNIT STRESS IN MEMBER "D" Sd' 25§2900 : 6,130#/sq. in. compression MAXIMUM UNIT.STRESS IN MEMBER "H" Sh: 423,700 - lO,560#/sq. in compression 4 ~44 MAXIMUM UNIT STRESS IN MEMBER "L" 81: 52%2220 = 13,380#/sq. in. compression UNIT STRESSES IN UPPER CRORD M NBERS IN MIDDLE TRREE PANELS (Members "P" and "T") CROSS AREA OF SECTION 2 plates 18" x E"- 18.00 sq. in. 4 angles 6" x 4" x 3/ "-QZLZQ sq. in. TOTAL- 45.76 sq. in. MOMENT 0F INERTIA OF SECTION _ IX-—2 plates : (2)(l/12)(§)(183)- 486 in.4 4 angles: (4) 24.5 / (6.94)(9.25 — 2.08)2: 1524 in.4 TOTAL: 2010 in.4 Iy~-2 plates: <2>(18)/ (18.00)(6.502): 765 in.4 4 angles: (4) 8.7 / (6.94)(6.75 / l.08)2: 1736 in.4 TOTAL: 2501 in.4 LEAST RADIUS OF GYRATION OF SECTION r:|I/A : 2010 : 6.61 in. 45.76 UNSUPPORTED LENGTH OF MEMBERS L- (11.1)(12)= 133" ALLOWABLE STRESS IN COMPRESSION FOR MEMBERS "P" AND "T" L/r- 132 20.1 Sc: 15,000 - (l/4)(20.l)2= l4,899#/sq. in. 6.61: TOTAL STRESSES IN MEMBERS Member "P": 607,500# compression Member "T": 607,300# compression MAXIMUM UNIT STRESS IN MEMBER "P" S = 607,200 = 13,280#/sq. in. compression p 45.76 MAXIMUM UNIT ST ”SS IN MEMBER "T" 3,: 607 200 : 13,275#/sq. in. 45.76 UNIT STRESSES IN VERTICAL MEMBERS AT END AND FIRST INTERMEDIATE PANEL POINTS (Members "A" and "E") CROSS AREA OF ECTION 0F MEMBER "A" L___LT ___J 1 plate ll" x 5": 5.50 sq. in. NM 4 angles 6" x 4" x §"= 19.00 sq. in. § TOTAL: 24.50 sq. in. I 1 L MOMENT OF INERTIA OF SECTION OF MEMBER "A" Iyn-Plate: (l/l2)(ll)(%)3 : 0.115 in.4 4 angles- (4) 17.4 / (4.75)(O.25 % l.99)2 - 165 in.4 TOTAL: 165.1 in.4 LEAST RADIUS OF GYRATION 0F SECTION"A" r- 165.1 = 2.59 in. 24.5 UNSUPPORTED LENGTH OF MEMBER "A" AND "E" L= (10.96)(12): 131 in. -45.. ALLOWABLE STRESS IN COMPRESSION OF MEMBER "A" L/r= 131 = 50.6 Sc- 15,000 — )1/4)(50.6)2= l4,360#/sq. in. 2.59 TOTAL STRESSES IN MEMBERS Member "A". 294,900# compression Iember "E": 246,300 # compression GROSS AREA OF SECTION OF MEMBER "E" 1 plate 11" x 3/8". 4.13 sq. in. A angles 6" x 4" x 7.16": 16.72 sq. in. TOTAL. 20.85 sq. in. MOMENT 0F INERTIA OF SECTION OF MEMBER "E" IY-—P1ate- (1/12)(11)(3/8)3- 0.048 in.4 4 angles- (4) 15.5 % (4.18)(0.188 / 1.96)2 = 139.2 in.4 TOTAL- 139.3 in.4 LEAST RADIUS OF GIRATION OF HENDER "E" I‘D 139.2- 2.58 in. 20.85 ALLOWABLE STRESS IN COMPRESSION 0F MEMBER "E" L/r- 121 s 50.8 Sc: 15,000 - (l/4)(50.8)2: 14,355#/sq. in. 2.58 MAXIMUM UNIT STRESS IN MEMBER "A" Sag 295,900 = l2,030#/sq. in. compression 24.50 MAXIMUM UNIT STRESS IN MEMBER "E" s : 246, 300 : ll,800#/sq in. compression 21'. o 50 TNIT STRESSES IN VERTICAL MEMBERS AT MIDDLE SIX PANEL POINTS (Members "I", "H", and "Q") GROSS AREA OF SECTION 1 plate 11" x 3/8": 4.13 sq. in. -46- 4 angles 5" x 3%" x 3/8": 12.20 sq. in. TOTAL: 16.33 sq. in. MOMENT OF INERTIAL OF SECTION Tye-plate: (l/l2)(11)(3/8)3- 0.048 in.4 4 angles= (4) 7.8 % (3.05)(0.188 / 1.61)2= 70.8 in.4 TOTAL: 70.9 in.4 LEAST RADIUS OF GYRATION OF SECTION r- 70.9 = 2.08 in. 16.33 ALLOWABLE STRESS IN COMPRESSION OF MEMBERS "I", "M", AND "Q" L/ra 121 . 63.0 sca 15,000 - (l/4)(63.0)2= 14,010#/sq. in. 2.08 TOTAL STRESSES IN MEMBERS MEMBER "I": 189,900 # compression Member "M": 134,200# compression Member "Q"- 78,9CO# compression MAXIMUM UNIT STRESS IN MEMBER "I" Si‘ 189,900 = ll,620#/sq. in. compression 16.33 MAXIMUM UNIT STRESS IN MEMBER "M" Sm: 1E%,§g0 : 8,220#/sq. in. compression MAXIMUM UNIT STRESS IN MEMBER "Q" Sq: 7§é9gg : 4,840#/sq. in. compression UNIT COMPRESSIVE STRESS IN DIAGONAL MEMBERS IN C NTER PANEL (Member "8") GROSS AREA OF SECTION 1 plate 11" x 3/8": 4.13 sq. in. 4 angles 5" x 35" x 3/8"- 12.20 sq. in. TOTAL: 16.33 sq. in. MOMENT OF INERTIA OF SECTION -47- Iy-~plate = (l/l2)(ll)(3/8)3: 0.05 in.4 4 angles: (4) 7.8 % (3.05)(l.80)2 e 79:82 In.4 TOTAL- 70.9 In.4 LEAST RADIUS 0F GYRATIOU OF SECTION “TE—9' ; 2.08 in. 16.33 UNSURPORTED LENGTH OF MEMBER (15.6)(12): 187 inches ALLONAELE STRESS IN CCMPRESSIQN 0F MEMBER "S" L/r= 1&2 - 90.0 2.08 Sc: 15,000 - (l/L)(9O.02)= l2,975#/sq. in. TOTAL STRESS IN COMPRESSION IN MEMBER "S" 8- 60,300# compression MAXIMUM UNIT STRESS IN COMPnESSION IN MEMBER "S" SS: 60,300 : 3,690#/sq. in. compression 16.33 -48- LAAIKUK'AIIOWABLE STIEES‘SES AND: 07 P0 SIBIS SIT IN TRUSS @143st MEMBER KIND OF ST MS ALLorAbLN SIILSS IN r‘OSSIBLE STFESS IN LBS PLR SQ. IN. LBS. P11” SQ. IN. A Compression 14,360 12,030 B None 18,000 0 C Tension 18,000 13,800 D Compression 14,897 6,130 B Compression 14,355 11,800 F Tension 18,000 8,200 G Tension 18,000 13,700 H Compression 14,897 10,560 I Compression 14,010 11,620 Tension 18,000 14,150 K Tension 18,000 14,000 Compression 14,897 13,380 n Compression 14,010 8,220 N Tension 18,000 13,600 0 Tension 18,000 8,350 P Compression 14,899 13,280 Q Compression 14,010 4,840 R Tension 18,000 14,900 S Tension 18,000 4,290 S Compression 12,975 3,690 T Compression 14,899 13,275 -49- MA.IMUM STRESSES IN L TERAL BRACIEQ HITIT [Jozafi/{t IIIIJIII| zur' > J'O' LR Height of structure as seen in elevation: 19.5 ft. Length of diagonals: 33.4 ft. WIND FORCES AND LATERAL VIBRATION FORCES APPLIED T0 STRU‘TURE wl- 30#/sq. ft. W1: (30)(19.5)(1)(1.5)= 878#/ft. W2: 150#/Iin. ft. w: 878 / 150= 1028#/ft. MAXIMUM STRESS IN A DIAGONAL LR: (1028)(50)= 51,400# Max shear: vmax= 51,300# smax. (51,400)(33.5)= 68,700# tension NET AREA PROVIDED IN A DIAGONAL 1 C7 2 angles 4 x 3s'x 3/8 - (2)(l)(3/8): 4.59 '"' ALLOWABLE TENSILE STRESS IN A DIACONAL S 18,000#/sq. in. AAXIMUM TENSILE STRESS IN A DIAGONAL 3. 68,700 : l5,000#/sq. in. 4.59 Since the shear in the center panels is less that that in the outside panels and the same area is provided in these panels, the maximum unit stresses in the bracing angles in the center panels are less than the above value. NECESSARY DEPTH OF SLAB AND AMOUNT OF REINFORCING STEEL -50- fcl- 2,500#/sq. in. fc- (0.4)(2,500)= l,000#/sq. in. fs: 18,000#/sq. in. IIINIIUM EFFECTIVE DLPTN 0F SLAB PROVIDBD: 6% in. EA OF STEEL PROVIDED PER FOOT 0F LENGTH %" square rods spaced at 4" A: (0.25)(l2/A)= 0.75 sq. in. MAXIMUM LIVE MOMENT IN SLAB [,0 ll 4.583 ft, spacing of stringers 0.7 s / 2= (0.7);4.583) % 2.00 5.2 ft., effective width of slab 33 ll t1) ll Maximum wheel load: 12,000# m. 12,000 - 2,310#/ft. 5.2 M: 1/4 wl- (l/I)(2310)(4.583)= 2,650 ft. lb. IMPACT MOMENT IN SLAB 4.58 / 20 -51.7% (51.7S)(2,650): 1,370 ft. lb. (0)(4- 58) ;fi20 MAXIMUM DEAD MOMENT IN SLAB Use average total depth of slab as 9" w: (9/12)(150)= 112.5#/ft. M- (1/10)(ll2.5)\4.583)2= 236 ft. lb. TOTAL MAXIMUM MOMENT IN SLAB 2,650 / 1,370 / 236: 4,256 ft. lb. MINIMUM EFFECTIVE DEPTH OF SLAB R: 173 M/Rb ( 256 12)- - 4 95 in. (173 12 STEEL AREA NECES SARY PER FOOT 0F SLAB p:.Olll A: pbd- (.Olll)(12)(4.95)= 0.66 sq. in. MAXIMUM FIBRE STRESSES IN STRINGEBS 9 Stringers--12" x 5" x 35# Rolled I-Beams Spacing: 8 @ 4'7" DL-CL- 36'8" Unsupported length= 11.1' CLPCL of floor Beams -51- NAXINUN LIVE NONENT FOR ONE LANE E. (12,000)(ll.l/2} 66,600 ft. lb. NIXIEUN LIVE NONEN‘ FOR ONE STRINGER C(reinforcec concrete slab): 1.0 N- Width of traffic lane 3 10.0 s 2.18 Spacing of stringers 4 - 50,600 ft. lb. E'. 0 M/N . 1.0(66 600) - (Z.IST' IL'IPACT KO L’ENT F OR OI‘IESTRII‘E 35; I. L g 20 . 11.1 20: 56.0 I 6L 20 66. M1. (36.0%)(30,600): 11,000 ft. lb. DEAD MOMENT FOR ONE LANE Using average depth of slab as 9 inches w(slab). (9/12)(10)(1)(150L: 1125#/rt. w(stringers)s {QQéSSQQIOE : 8&#/ft. 56 2 TOTAL w. 1211#/ft. N. 1/e wlzs 1/e(1211)(11.1)2. 16,650 ft. lb. DEAD MOMENT FOR ONE STRINGER E'. (1.0)(18 650). 8,540 ft. lb. m) T OTAL 1m DIUM MOMENT IN ONE STEINOEE E. 50,600 / 11,000 / 8,540: 50,140 ft. lb. ALLOWABLE TENSILE STRESS IN BOTTOM OF STRINGER st. 18,000#/sq. in. AIIDWABLE CONGRESSIVE STRESS IN TOP OF STRINGER L b. 1101 12 C‘ ' / $5.078 ) g 26.25 Sc. 18,000 - 5(L/b)2.14,550#/sq.in. -52- ILAXILTUM COLIPRESSIVE AND TENSILE STRESS IN STRINGER 3. Mc . I§0 140)(121L4 .88) e 12 ,920#/sq. in. tension I W? and compression mummdmmknm EMSEINNIO.S MAXIMUM.LIVE SHEAR FOR ONE LANE v. 24,00O# N‘"IMUM LIVE SEEAR IN ONE SIRINOER O. 1.0 N. 2.16 l v . (1.0)(24 000) a 11,OOO# {$.IE) IMPACT SHEAR IN ONE STEIN ER (56.0%)(11,000). 3,960# DEAD SHEAR FOR ONE LINE w(tote1). 1211#/ft. 1 v =(1211)(11.1). 5080# '1‘ OTAL DIME-ma SEEAR IN ONE Sr “R INGER v. 11,000 / 5,960 / 5,030: 18,040# AIIOWASLE UNIT SHEAhING STRESS IN W+B Clear distance . 9.75. 22.8 which is less than 60 Thifikness .125 v. 18 040 .- 3,520#/sq. in. IIZ.OO)IO.4§§5 I'M II-EUI'II LIVE LOAD AND DJIPACT IIEOLCENT IN FLOOR B11113 /Z’ooc' ’2000‘” 12,000? (z’aoot 12,000: ,2 can” I . , .3 7 ,6; , 3' 6 4' .z ; ‘1 I I t J ’ I 25'! {-f Fuss A NAIINUL: LIVE MOMENT IN FLOOR BEAN N1. 0 (12,000)(2 / 8 {11 K 17 I 20 % 26): (RR)(25) -53- RR. (12,900)Ls4). 40,300# (257 LR. (6)(12,000) - 40,300 - 31,700; Mmax- (51,700)(11) - (12,000)(3 / 9) mmax. 204,700 ft. lb. Since three lanes are loaded to obtain this maximum bending moment, only 90% of the total moment is used in the design. Mu (90%)(204,700)- 185,000 ft. lb. IMPACT MOMENT IN DEEMED IATE FLOOR BEANS I- L i 20 n 25 f 20 I 26.5% L O 5 20. M: (26.5%)(184,000) M: 48,700 ft. lb. IEPAOT NDNENT IN END FLOOR BEANS I- (2)(26.5%)- 53.0% Mb (53.0%)(184,000): 97,500 ft. lb. MAXIMUM DEAD MOMENT IN INTERMEDIATE FLOOR BEANS 4“)” 5,390" 5390 €330 6 390 6390 5330 (390” 99/0 ”' ff -$flflV‘ $52!; fldzsiitsusi 4w33i {fasi‘asasi 1mnn4agv’ 6333’ I \25300' 6133' 33am" Mr. .f .67..» am". y, V/I: 3538/0" Assume weight of slab as uniformly distributed to the strin- gers. Assume weight of walks, railing section, and railing posts as being carried entirely by the outer stringers. WEIGET APPLIED TO EACH FLOOR BEAM THROUGH EACH INSIDE STRINGER Weight of slab-fiLg%§%)(ll.l)n 6,000 lb. Weight of stringer-~(35)(ll.l)- SQQ_lb. TOTAL. 6,590 lb. WLIGHT APPLIED T EACH FLOOR BEAM THROUGH LEIGH OUTSIDE STRIP-3 mi -54- Weight of slab-~6000- 3,000 lb. ‘"§“ Weight of stringer--(55)(ll.l)= 390 lb. Weight of sidewalk—-(535)(ll.l)= 3,720 lb. Weight of railing section--(44)(ll.l)s 490 lb. Weight of railing posts-- 810 lb. TOTAL. 8,410 lb. TOTAL'WEIGHT 0F FLOOR BEAM 4 287- 114#/rt. EOTEV MAXIMUM DBAD MOMENT IN INTBAMBOIATB FLOOR BEAMS LR- (5.5)(6,95O) # 8,410 ; (4,287). 34,810# M. 456,000 - 175,600 - 154,200 - 20,200 m- 86,000 ft. lb. L'AXIMUM FIBRE STRESSES IN INTEREEDIATE FLOOR BEAMS TOTA1.MAXIMUM MOMENT IN INTERMEDIATE FLOOR BEAM Live moment 184,000 ft. lb. Impact moment 48,700 ft. lb. Dead moment 86,000 ft. lb. TOTAL. 318,700 ft. lb. ALLOWABLE TENSILE STRESS IN BOTTOM OF INTBBBBDIATB FLOOR BEAM st. 18,000#/sq. in. ALLOWABLB COMFRBSSIVB STRESS IN TOP OF INTBBLBDIATB FLOOR BEAM L/b. :25 12). 25 so: 18,000 - (5)(L/b)2 2.0 so- l4,885#/sq. in. MAXIMUM COMPRESSIVE AND TENSILE STBBSS IN IATBBMBBIATB FLOOR 3. Mc/I- 518 700 '12) 10.44) 1"'TE§B%.3) "“ -55- BEAM 8: 13,370 #/sq. in. tension or compression 1':le 11'2de DEAD MOMENT IN END FLO OR BEAMS 3' F p g . 310m afar 3185 538! Tums” sum“’,iru’ ,fira' gznf‘ 250.90” 25030.? WEIGHT APPLE!) TO EACH END FLOOR BEJ'EM TFiOUGH EACH INSIDE S T R IN GER Weight of slab--(4320)(ll.l)= 3,000 lb. Weight of stringer--(35)(ll.1): 195 lb. Weight of expansion angles--(1525)- _ 190 lb. TOTAL 2 5,585 lb. WEIGHT APPLIED TO EACH END FLOOR BEAE:TBBOUGH EACH OUTSIDE STRINGER Weight of slab--SQOO - 1,500 lb. Weight of stringer--(35)(ll.l/2)z 195 lb. Weight of sidewalk--(335)(ll.l/2)- 1,860 lb. Weight of railing section-~(44)(ll.l/2). 245 lb. Weight of railing post-- .lLéZQ lb. TOTAL: 5,270 lb. TOTAL WEIGHT OF END FLOOR BEAI‘JI AND CONCRETE AROUND IT - 15,915. 422#/ft. 37.67 MAXIMUM DEAD I:ZJI‘~.EITI IN END FLO OR EMJS .l§§218.. 25,090# M- 514,OOO - 95,100 - 96,700 - 75,000 M: 49,200 ft. lbs. LR. (5.5)(5,5857 % 5,270 / -56- MAXIMUM FIBRE STRESSES IN END FLOOR BRAKE TOT$1.MAXIKUMIMOMENT IN END FLOOR BEAM Live moment. 184,000 ft. lb. Impact moment. 97,500 ft. lb. Dead moment- 49,200 ft. lb. TOTAlm 330,700 ft. lb. ALLOWABLE TENSILE STRESS IN BOTTOM OF END FLOOR BEAM St;- 18 ,OOO#/SQO in. .ALLOWABLE COMPRESSIVE STRESS IN TOP OF END FLOOR BEAM L/b- 25 12): 24.9 2. 4 ) s0. 10,000 - (5)(24.9)2= 14,900#/sq. in. MAXIMUM COMPRESSIVE AND TENSILE STRESS IN END FLOOR BEAM 3. M0. (550,700;§12%g10.44) 17‘ 5 . S. 12,520#/sq. in. tension or compression MAXIMUM SHEARING STRESS IN IBTERMEDIATE FLOOR BEARS MAXIMUM LIVE SHEAR IN ONE FLOOR BEAM ”goo" /% ago [3000 I “a [2.00“ / 00¢ 6” L3' 1 1§’. 1 3“ l 6 ’ 41’; 23" LR RR LR- (12,000)(25 £_19 i 16 / 10 £_7 { 1). (12,000){%§g 25 LR. 57,400# vmax. 57,400# Since three lanes are loaded to obtain this value, only 90% of the maximum.need be used in design. V. (90%)(57,400). 55,550# -57- INRAOT SHEAR IN ONE INTERLEDIATE FLOOR BEAN (26.5%)(35,650)- a.920# MAXINUN:DEAD SHEAR IN ONE INTERMEDIATE FLOOR.BEAM v. 24,810 - 8.410 - 6,390 - (114)(6.33) v. 19,290# TOTAL IMIIIUN SHEAR IN INTENSEDI TE ILOOR BREE 33,650 ; 8,920 f 19,290. 61,860# ALLOWABLE UNIT SHEARING STRESS IN WEB OE BEAN Clear distance - 20.875s 44.7 which is less than 60 “Thifikness 6.455 v. 12,000#/sq. in. IleXII‘JRH-fi UNIT SHEARING STRESS IN WEB OF llfl‘ERP-‘EDIATE FLOOR 331.5111 v- 61 860 . 5,500#/sq. in. ( . MAXINUMZSHEARING STRESS IN END FLOOR BEAN NAEIEUNLLIVE SHEAR IN END FLOOR BEAM v- 53,650# INBAOT SHEAR IN END FLOOR BEAN (53.0%)(33,650)- 17,840# MAXINuszEAD SHEAR IN END FLOOR BEAN; v. 23,090 - 5,270 - 3,383 - (422)(6.33) v. 13,760# TOTAL mmem SHEAR IN END EIOOR BEAM 33,650 } 17,850 / 13,760. 65,250# ALLOWABLE UNIT SHEARING STRESS IN WEB 0F BEAM Clear distance a 20.875: 41.0 which is less than 60 Thickness . v. 12,000#/sq. in. TilAXDflTUNT UNIT ‘3 MING STRESS IN WEB OF END FLOOR BEAM -58- v. 65 250 . 5,30 fi/sq. in. ENZAJCDEUM FIBRE STEESSES DUE TO FLOOR BEANS AND STRINGERS IN POUNDS ALLO‘T AB LE L'IAX IIITUM UTE IT 8‘11"“55 UNIT STRESS IIN COIR’ERBS- IN COLTRI'SS- SION SION STRINOERS 14,550 12,920 INTERNEDIATE FLOOR BEANS 14,235 13,370 END FLOOR BEANS 14,900 12,520 I‘AXDEUTJI SILF’ARWG STmSSES IN SENDING IN PER SQUARE INCH ALLONABIE IEIEIIEI LTIIT STRESS UNIT STRESS 11V TEN S ION IN TENS ION 18,000 12,920 18,000 13,370 18,000 12,520 ‘JEEBS OF FLOOR BET HE'S AND STRINGERS IN POUNDS PER SQUARE INCH ALLOWABLE UN IT SEEPJJNG STRESS STRINGERS 12,000 INTEPILED LATE FLOOR BEANS 12,000 END FLOOR BEANS 12,000 CONCRETE BEARING AREA. Size of lead bearing plate-~22" x LUIXII‘IIIVI DEAD LOAD REACTION R- 196,90Q# lx'AXDIUIu‘I LIVE LOAD AND III'ZPACT REACT ION R. 98,000# TOTAL MAXDIUM REACTION R: 196,900 { 9S,OOO. 294,900# -59.. MAX EMA UN IT SI-IEARING STRESS 5,500 5,300 2'5" RLLONABLB BBARING STRESS IN OONORBTB rc'. 2,500#/sq. in. s- (0.25)\2,500). 625#/sq. in. NININDN CONCRETE BEARING ABBA NBOBSSARY 294,900 g 472 sq. in. 625 CONCRETE BEARING LREA PROVIDED 22 x 23- 506 sq. in. -60- ,1, , ., . 3:» :flso an? n ww.m<¢m_4 >tmmm>_23 mh