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HomeMy WebLinkAboutFOOTING & FOUNDATION DESIGN - 95-00018 - Taylor Chevrolet - Expansionq F O LAO, +/Iwmlr f5jrewm� AAo. CtQ � 15 tv/ J6 ls. c I 5 Fr 4f Al OFF, RISA -2D W-111more Engineering 442 North Main St. Sountiful, Utah 84010 -up (R) Vers ion 3 * 0 3 TAYLOR CREVROLET REXBURG �•, r. — �— � i � — � �a,� _ _ � � ,� � � tri � .� •� � Lam! T� .,�. � � rr �. — +i _ � �if� err � Load Combinatiorl is 8 WIND React ions UL 14 '95 14: 26 - no" — — — j- � por, MMM6 Fw- — — — 6-1 -A MR — � _ � � %_.,. _ _ � M F._ _ _ &M %MF _ _ _ _AA � r-- — — _6 � r— — — -LA -6A � — � — " � J�- — — — --dL Node Global X Global Y Moment _�------ — ----- — ----(x)- ----{K)-- -Lu ------------(K- ft) --- - "Tr ---- �. -5.08500 -1,69500 0-.00000 51.69500 1.69500 0.00004 Totals - 6.78 00 0 0.010000 0,00000. Load Combl'naLion is I DEAD + LIVE, Reactions iii PM T — — A� a w -F — — . AM Tr — `, — J6k � Oil —. — ,,w � 1W :T — _ _ � _ — _j s m1 _ _ _ iii _. p"r — _, ii ._ .P" — L& is ! � k- 23ode Global X Global Y moment 1 5 Totals (K) 6. -6-00000 0-.00000 00000 (K) 12. 12.40000 24-.00000 00000 (K -ft) �?-r-�--AMMMM 0.00000 0.00004 0.00000 f LA -h RISA -2D IN Wil 1more Engineering 442 North Main St, Bountiful, Utah 840].0 (12) Version 3.03 112 P17 JUL 14 '95 14:26 Job Page Date TAYLOR CHEVROLET REXBURG I ! ZM�1 e`i 'RRTkbe OEM S Vie' 71ii g�Y' _'-.� + ' ` -: - " � �!�F = = f = - =. . , � ALL, = ;M M - aL r� � 'For d 77i. p i-.� �. - •- �_ -� �� ENVELOPE SQLCTTION Member Section Results 1. a MW PEW i Ww � ME; i f l i 7 i ■fai -W= '=F W" W" P9"R Yrt Nodes No I j I -End , in) LC(KI 12.85 6 1.31 2 3.58 2 -8.84 7 x.00 6 -0.00 7 0. 000 1 01000 i 6.85 4 -0. 19 3 12.85 6 7. 3 1 2 102.71 6 -2.92 2 0.000 1 0.000 1 6. 8 5 4 -0.19 3 1.69 3 -1.69 2 0.00 9 0. 00 2 0..,000 1 0.000 i 12.$5 4 1.31 3 &.85 4 -0.19 3 1p2.71 4 -2.92 3 0.000 1 0. 0 0 0 1 - - - 'L- � �% -AL -b6 A" -L4 6M M& � � ( X I Kft 171 z 3 n I- x Me 4- 2 A V M D 3 A V M JJ 4 A V M D 5 A V M D ENVELOPE SOLUTION AISC Carie Cheeks Member Quarter Points 1/4 1/2 3/4 Kf t , in) LC (K, 7.2. 85 6 1.3l 2 1. 8 9 2 -7.70 6 30.45 b -10.7 2 0, 012 7 -Q.009 2 6.$5 4 -0119 3 9.85 6 0 . 56 2 60.15 6 -5.41 2 -0.042 3 "0. 016 4 6.85 4 -0. 19 3 0.94 3 -3.85 4 9. 87 5 -4. 95 3 0,022 4 0.005 3 12.85 4 1. 31 3 6.85 4 -0. 19 3 7 7. 0 3 4 -2.19 3 0.411 6 •0.002 2 Kfit,n) LC (x, 12.85 6 1.31 z o. 19 z --6.85 6 57.71 6 -14.17 2 0,021 7 -0.018 2 6.85 4 -0.19 3 6.85 6 -Q.19 2 2 $. 8 6 6 - 7. 09 2 -0.006 3 -0.036 4 6. $ 5 4 -x.19 3 0.19 3 -6. 8 5 4 28.86 4 -7109 3 0.044 4 0.010 3 12.8 5 4 1.31 3 6.$5 4 -Q. 19 3 51.36 4 -1.46 3 0.618 7 -o.00s z Kf L in) LC (A 12.$ 5 6 1.31 2 -1.50 2 -6.04 6 81,.80 6 -11. 73 2 0.026 7 -0.025 2 6.85 A -0.19 3 3.1-85 5 -0.94 2 9.87 7 -4.95 2 -0. 012 3 -0.057 4 fi.85 A -0-19 3 -0.56 3 - 9.8 5 4 60.16 4 -6.41 3 Q.063 6 0.015 z 2.85 4 1.31 3 6.85 4 -0. 19 3 25.68 4 -0.73 3 0.024 7 -0.05 2 J - End Kf t., in) LC -- 12.85 6 1. 31 2 0.19 3 -6.85 4 102. 71 6 - 2. 92 2 0.028 3 -0.034 5 6.85 4 -0.19 3 1.70 7 -1. 6 4 2 0400 1 -o.00 6 -a.o1a 3 -0.079 4 6.8 5 4 -0.19 3 -�..31. 3 -12.85 4 X02.71 4 -2.92 3 0..,079 fi 0,017 2 12.85 4 1.31 3 6.85 4 -0.19 3 0.00 7 -Q_00 6 0.03D 7 -0.024 2 �, .- -. - - •- - - d, Idb #� LLL a r+. i� i ow mw m -f Nodes Member Quarter01n No T J_ Max 1 C C 1/4 Ic 1c 3/ 1 C S ear 1c rem" M" " -p MW ""W" Y!! 1t i Fmf. i � Els ! it Fid k=. •i v. ,., a..LL - ^a S i MR 1111L i i .Ew i � 71f, � 77'7 "fi 7T TW VIA' rw -W A f I I - 2 - Not Calculated 2 2- 3 Not Calculated 3 3- 4 Not Calculated 4 4- 5 Not Calculated RISA -2D (R) Version 3.03 Willmore Engineering 442 North Main St. Bountiful, Utah $4010 TAYLOR CHEVROLET REXBURG IDAHO 112 P16 JUL 14 '95 14. 25 Job W -'r rp Page Date Dynamic Analysis Data Number of modes (fireVencies) Bacic Load Case for masses BLC mass direction of actionAccelerat "ion . fr Gravity 3 None X only 32.2Q ft/sec**2 ENVELOPE SOLUT Nodal Displacements �.► y.. i �+ _ - _ 1 .amu a ww M- - _ _ - - -- �. �+ � i �I rrr - - ....r. - 1.M i Kik � 1'T ._ � z�. � .� � � � Node Global X Global Y Rotation - - - - ------ - - -- -(iri)------LC----------(in)------LC----------(rad)----�LC- 1 max 0. 00000 2 -0-00000 2 0.00-027 7 Mill -4.00000 7 -0. 000(30 6 -0, 00021 2 2 max 0403443 5 -0.00162 2 0.00000 3 min -0.02791 3 -44-01595 6 -0.00030 4 3 max 0.02757 2 -0.02245 2 0.00,050 4 min -0.02767 3 -0 . 9310 6 0"00011 3 4 max. 0.,,02370 2 -0.00162 3 0.00030 6 min -0.03022 7 -0.01595 4 -O.00001 2 5 max 0.00000 4 - 0. 0 0 0 0 0 3 0.00016 3 m7.n -0.00000 3 -0.00000 4 -0.00022 S ENV2LOPE SOL ION Reactions No -de Global X G1oba]. Y Moment - --------- - - - - -- (x) - --- - - LC - - (K) ------ LC ---------7- {R -fC)----LC- 1 max 8. 83500 7 12. $450 6 0.00000 1 min -3,58500 2 1..30500 2 a . 00000 1 5 max D_19500 3 12.$4750 4 0.00000 1 min -6.84750 4 1.30500 3 0,00000 1 Load Combination Self Wt SLC BLC SLC BLC BLC W E No. Description Dir Fac Fac Fac Fac Fac Fac DYITA S V 1 DEAD + LIVE 1 1 2 1 Y 2 DEAD + WIND 1 -1 3 1 Y Y 3 D EAD + WIND - 1 -1 4 1 Y y 4 DL + LL + 1/2WIND 1 - 1 2 -1. 3 .5 Y y 5 DL + 1/2LL + WIND 1 -1 2 -.5 3 1 Y Y 6 DU + LL + 1/2W- 1 -7 2 -1 4 .5 Y Y 7 DL + 1/2LL -r W- 1 -1 2- .5 4 7 y y g WIND 3 1 Dynamic Analysis Data Number of modes (fireVencies) Bacic Load Case for masses BLC mass direction of actionAccelerat "ion . fr Gravity 3 None X only 32.2Q ft/sec**2 ENVELOPE SOLUT Nodal Displacements �.► y.. i �+ _ - _ 1 .amu a ww M- - _ _ - - -- �. �+ � i �I rrr - - ....r. - 1.M i Kik � 1'T ._ � z�. � .� � � � Node Global X Global Y Rotation - - - - ------ - - -- -(iri)------LC----------(in)------LC----------(rad)----�LC- 1 max 0. 00000 2 -0-00000 2 0.00-027 7 Mill -4.00000 7 -0. 000(30 6 -0, 00021 2 2 max 0403443 5 -0.00162 2 0.00000 3 min -0.02791 3 -44-01595 6 -0.00030 4 3 max 0.02757 2 -0.02245 2 0.00,050 4 min -0.02767 3 -0 . 9310 6 0"00011 3 4 max. 0.,,02370 2 -0.00162 3 0.00030 6 min -0.03022 7 -0.01595 4 -O.00001 2 5 max 0.00000 4 - 0. 0 0 0 0 0 3 0.00016 3 m7.n -0.00000 3 -0.00000 4 -0.00022 S ENV2LOPE SOL ION Reactions No -de Global X G1oba]. Y Moment - --------- - - - - -- (x) - --- - - LC - - (K) ------ LC ---------7- {R -fC)----LC- 1 max 8. 83500 7 12. $450 6 0.00000 1 min -3,58500 2 1..30500 2 a . 00000 1 5 max D_19500 3 12.$4750 4 0.00000 1 min -6.84750 4 1.30500 3 0,00000 1 RASA -2D (R) Version 3.03 Willmore Engineering 442 North Main St. Bounti flil, Utah 84D7.0 TAYLOR CHEVROLET REXBURG . IDAHO 112 P JUL 1 a 95 f 1 �® — �y i`s ArT — T� �.` _�. it .!w!!1 — �, ilk+� s� �..+rl�l �i 77� •—. L! ����� — .14 'Tr �_ —. �iL iP."' —. �L Trr' —• �'ii'�' .�_ ya if�l� ifs � — M mpm- � — MW M r - U MC " — � _ Rwa i — — 40S mi � R6L » "— — � A" M wr � i " = tiT r-* � — M i - � h-- r ` 1W i --R d.- IM i � — J a dM J �-- --r _ -li . wr � — _ LU � qu- — I J' Unbraced Lengths K Factors Bending Caere No Node Node Lb - in Lb - out L c In Out Cm Cb Rr' ALL ALA — f t 4— MkA ( ft ) 6-6 (ft) ANN .6U 1 1 - 2 2 2 - 3 3 3 - 4 4 4 - 5 � — — — &W i . _ — — — — .„A "W 1r4 BLC Basic Load Case Load Total No. Description Nodal Po ir 1� i e* - 1 1) FAD LOAD 2 2 LIVE LOAD 2 3 WIAID LOAD + 7 4 WIND LOAD - 1 Member Distributed Loads,3LC 1.- DEAD LOAD Memb I J Start End Start End --� No Node Node Dir Magnitude Magnitude Location Location (K/f t F) bon - kmr (f t) —, LM (f t)---- 2 2- 3 Y 0.200 0.200 0 . 0 0 15.400 3 3 - 4 Y O.ZQO 0.200 0.00 15.000 Member D11 s rid. Loads. BLC 2 LIVE r --- — — — M" i w EJB �1 — — sryy A� ILII A� 7R — �� �. �YL A %w AR — — -- .. .. Mems T J Start End Start End ,.� "►aC;: XvL)atj WZr Magr]Ztt1ae Magnitude Locat jo� Location IM MW Wff p - ft I F) &= 2 2 3 Y D.600 3 3 - 4 Y 0.600 K/f t I P) � rrh, — — — — — — — ( ft RM, — — -L. T -T -- 0.600 0 .0 0 0 15.000 0.600 0.,000 15,1000 Member D-istrl'buted Loads. — s 4-6M emb I Start End Start End No Node Node Dir Magnitude t e L �1Location F) =4 AMR W" (K/f t I F) - -6J A.Nf t ) — — — -&A A.6L am M � T., ( t ) — — — "T 0,5452 0 i 0 0 0 .0 0 F Member Distributed - - , - - - - �- — "4 &AU fa it i i R i tir� Prv' —r � 1 9— --% MCnLmb I LT Start End SLart End No Nocle Node Dir Magni'Lude Magn:I'Ltude Locat 110n Locatiozi .� t) - - - (f t) mO.452 &&0#452 RISA -2D (R) Version 3. 03 wi'llmc)re Eng ilneeri 9 ng 442 North Main St. Bountiful, Utah 84010 TAYLOR MEVROLIMT RPXBURG, IDAHO 112 P14 JUL 14 '35 14:24 Job Page Date —� � � r� �L � � �� �L.Y' i �r � � � �� !'MR �� � � +�1,1-� � Ir � � J � �� � �-_ '� �jl� � � i � � ,� �i ;fi�l ar} �a �L � `rte � �• �4 � '1"�} � � r�rL � rr � �_ �L rY �" � � �-+�F i T.°" —r � �aLe s � —, �— yam. Units Option US Standard AISC Code Checks 9th Edition ASD Shear Deformatiori: No P -Delta ]�tffects- + Redesign No Edge Forcert2 NCS 1. 333 » i T — i i P=F M .. — � — — ZL iii '*T — — — -" a a w "IT — — — r _ i W" I'M I'M �-- — ." Am% Ilii TR — — � �.— -&A i P"r — — '—. — A&& In WI Node Boundary Conditions No X-Coord Y Coord X-dof Y-dof Rotation -------- —-(ft)--------(ft)-- �--(in,K/in)----(in,K/in) -�- (r.K-ft / r 1 D.00 0.00 R R 2 0.00 15.00 3 s.00 15400 4 30. 0 0 15.00 5 30.00 0.06 R R Temp . ]Elastic 0..00 - ^ �i iZL "m _ wr Tr Weight 0.00 Label Modulus O,aO 0.00 f}i TTT �'t-- - r .r - -s - -. (Ks:',L') -i 1J— ��'i 0. 00 ]Elastic Am ISA ill vrr FE - F� -, ..�6 _ _ 7TT �_ �� Poisson s Thermal - ^ �i iZL "m _ wr Tr Weight z,w i1 i Yield Stress Label Modulus F P Ratio Coef EJLC'entity (F y) f}i TTT �'t-- - r .r - -s - -. (Ks:',L') -i 1J— ��'i _ - - s .- -s � T7TL � ,F� .. � �� i �'(P) � � ` �- (K/f1. - c 4 �a (Ks 1 — -ja STEEL 29000, 00 0430000 0.65000 LL. — :.iY. Section Database Matl. Area Moment of As Y/ 9F 9r Label Shape Set Tnertia Coef — -.:. ,.. , "A . ,ar Jon it ._ MEN _ � i' i Ain MLT I"Rr TIT .P"+r — — — — ` — — !� (in'2) 14) STEEL 5.00 10,000 F. 000 ARCH 1.20 .� W+4 "a _ JEM a .ice !!� Yi' �. i`r rwe — — _ — — — ,-•A — � � , � " i M i M M = Moi TA' � ---0 "'. .W.4 .a Releases End offsets No Node Node Section x y z xyzSL:sc Sway I j Length mmF d_' s _ i Ir'hlg TR 1T AML i n) (I"n) - - -6 ,, ( f t ) 2 ARCH 15.00 2 2 - 3 ARCH 15,400 3 3 - 4 ARCS 15*00 4 4 A= 5 ARCS 15.00 PROJ8CT NAME TAYLOR CHEVROLET PROBLEM 7 . D. HORIZONTAL SLAB AT COLUMN CONCRETE BEAM As*** AV Mu vu M u = Fy = Y'r C = bTom - d= ra = 77..7 60 4 8 24 0.9 ** AsRegd ==0,744947 P == 0.0039 (200/Fy) (0. 75pb) min min max a 112 P13 JUL 1 '95 14:24 TANNER & ASSOCIATES ENGINEER:DAV17J R. SMITH DATE -R Jul -9S MOMENT CAPACITY TEN$ION REINFQT2CTNG ONLY (k,z'.p * f t) (ksi) (ksi) (inch) (inch) (f actor) (sq. inch) (ratio) /Fy As Min f, 11 4 A s max 59.558$2 -1296 932.4 AsRecrd =-0. 744947 (-root) _= 0.85 1.933254 Mu min ==54.69647 0,64 Mu min ==67.087175 = =x.104979 Mu max ==359.7036 (sc�.inch} (kl"p* f t) actor) (n -t aX3 S) (inch)