over time repetitive axial loading will increaseover time repetitive axial loading will increase

*'"# [5TiEc1-d0I4Yf8F The creep coefficient (t,t0) was calculated by Eq. That information is not)Tj 0 -1.16 TD (provided in your text so we must make an assumption. (1989). )Tj 2.8516 0.763 TD 1.6615 Tc (. !!!!WBP:sc%D;q/!!!EA!!!!EBPhj9&ReK9!!!Ee!!!,BCi!!<3$!!!t2!!! This category only includes cookies that ensures basic functionalities and security features of the website. )Tj /F9 1 Tf -3.875 3.6953 TD 3.0239 Tc [(==)-1140.6(=)]TJ 11.9427 -0.763 TD 0 Tc (-)Tj -12.3229 -2.1693 TD (=)Tj 2.9948 -0.763 TD (-)Tj /F7 1 Tf -1.7734 3.6953 TD 2.9059 Tc (KK)Tj 5.5208 0.6276 TD 0 Tc (P)Tj -0.9531 -1.3906 TD (A)Tj 3.7187 0.763 TD (K)Tj 2.5078 0.6276 TD (P)Tj -1.5938 -1.3906 TD 0.3861 Tc [(tW)-827.8(D)]TJ -9.5807 -2.1693 TD 0 Tc (K)Tj 2.9609 0.6276 TD (P)Tj -2.0443 -1.3906 TD (W)Tj 6.999 0 0 7 262.073 629.363 Tm (nom)Tj 6.4018 -1.3125 TD (reduced)Tj -12.5313 -3.7187 TD (all)Tj /F3 1 Tf 21.8527 3.7232 TD (1)Tj -15.9911 -5.0268 TD (1)Tj 11.998 0 0 12 263.791 604.707 Tm (16)Tj 1.013 -1.3906 TD 0.25 Tc [(02)250(5)]TJ /F10 1 Tf 12 0 0 12 90.001 531.137 Tm 0 Tc (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD 0.0002 Tw (We must first choose a W)Tj 6.96 0 0 6.96 232.321 528.737 Tm 0 Tw (1)Tj 12 0 0 12 235.921 531.137 Tm 0.0001 Tw ( to start with and find the K value corresponding to it. Eom, TS., Kim, CS., Zhang, X. et al. Eurocode 2: Design of concrete structuresPart 1-1: General rules and rules for buildings, BS EN 1992-1-1: 2004 (p. 2004). It covers design for strength, stiffness, and stress)Tj 0 -1.16 TD 0 Tw (concentrations. There is also strong evidence that repetitive load-ing affect both discs and vertebrae, and can cause path- This is approximately 42% of the yield stress for compression/tension. So here we need only be concerned with normal forces. :9c1!/LWA!Fu=G!0.%8!IOn1!2]gh""=Ck"tBfl!QbCW "D&Kq/T"9A?B"2Oh""T\E"+9]I[ BT /F4 1 Tf 12 0 0 12 90.001 709.217 Tm 0 g BX /GS1 gs EX 0 Tc 0.0001 Tw (From the graph, you can see that 1.75> /ExtGState << /GS1 14 0 R >> >> endobj 39 0 obj << /Length 3874 >> stream In S.I. The ratio of lateral strain to axial strain was more than 0.5, even closes to 1. 'Dha Besides highlighting the oftentimes neglected role of repetitive subpathological axial load forces in traumatic . The test results show that the . !LWu5!RLl2!^Qle!c%l+")%dV"2+h("@<5i"EO]u"bm2=#3c%grl"f`rqHFJs+UMN *)]TJ /F4 1 Tf 12 0 0 12 90.001 429.857 Tm 0 Tc (Lets start with W)Tj 6.96 0 0 6.96 173.041 427.457 Tm (1)Tj 12 0 0 12 176.641 429.857 Tm (=1 inch. We will use the reduced)Tj 0 -1.16 TD 0.0003 Tw (area for the area. Terms and Conditions, !&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8 6s0L_YV&jIYWPcd=Kr/=7C`B5?pn-J.k-JW,>Zt7@!1sR6VDc"U*lg!"&r6j8f5u#R1In!X$(:0`VL\R/no? !>be(!iH,s!=JqA"?luk!$MH7!3QED!IXsU!_!(h$Mt*f!@n1G!NH-T! =Lf8t4!>QS!N6,$!"1;[YRi$GYRr*H!%W/6F*.I"7;5.YBgbC(7! There is also strong evidence that repetitive load-ing affect both discs and vertebrae, and can cause path- It is important because it helps us locate the centroid of an object. 18CTAP-C129746-02). Six cantilever column specimens were concentrically or eccentrically loaded for 64days and the long-term deformations depending on the magnitude of axial load and eccentricity were investigated. )Tj /F4 1 Tf -17.6328 -1.9833 TD (4. Axial loads are applied along the longitudinal or centroidal axis of a structural member. !*TBD!/U\R!)`e#!(6gO!?(pE!&">G!!<4p!6kK[! (1991) Creep Buckling of uniaxially loaded reinforced concrete columns. If your restricted ankle issues stem from joint mobility problems, foam rolling and stretching won't help. Plus, the older you get, the less tolerant your body becomes to explosive exercises such as squats, cleans, deadlifts, and overhead presses. From recently published )Tj -6.0807 0.6276 TD 0 Tc [(1)-250(7)0(5)-942.7(0)-250(7511)]TJ 2.4714 -1.3906 TD (2)Tj 5.9505 0.763 TD [(0)-250(080)]TJ /F4 1 Tf 2.3542 0 TD 0.0001 Tw (, then use the area found to find the deformation)Tj -16.5 -1.88 TD 0 Tw (of that section. Repetitive axial spinal loading affects the disc height (Gooyers et al. !!<9t!42_b"60B6!,DYg! A force can act on an object in various ways. A non-osteoporotic adult presented with multilevel compression fractures at the apex of the thoracic kyphosis after strenuous rope jumping. A factor of safety F.S. 2023 BioMed Central Ltd unless otherwise stated. *<7/_O91IC*<7/_O0\R%+1M?=Z6m1*5nsEe!$27D!$;5%!%%^m!$;5$!-88D!$;5! There are several reasons to research the effects of axial twist exposures and the resulting loading on the spine. )Tj /F10 1 Tf -1.5 -1.14 TD 0 Tw (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD 0.0002 Tw (Fourth, we will determine the depth of the weld to prevent shear tearout. This can cause deformations in the object, which are a result of the stress caused by the load. The elastic lateral displacement 0 of each column specimen was used as the values measured by the LVDTs, shown in Fig. )Tj /F6 1 Tf 0 -2.2 TD 0.0001 Tc 0.0006 Tw (Strength Design of Bracket)Tj /F4 1 Tf 0 -1.4 TD 0 Tc (1. )Tj 0 -2.34 TD (FBD:)Tj ET 144.241 194.657 m 144.961 194.657 l 145.201 180.257 l 145.201 179.537 l 144.481 179.537 l 144.241 193.937 l f 140.881 180.737 m 144.721 172.817 l 148.561 180.737 l 140.881 180.737 l f* 0.72 w 162.121 362.657 m 162.121 347.777 l S 165.841 361.937 m 162.001 369.857 l 158.161 361.937 l 165.841 361.937 l f* 126.121 362.657 m 126.121 347.777 l S 129.841 361.937 m 126.001 369.857 l 122.161 361.937 l 129.841 361.937 l f* 1 g 133.681 194.657 20.88 157.68 re f 133.321 352.697 21.6 -158.4 re S 90.001 338.417 28.8 21.6 re f BT 12 0 0 12 97.201 345.857 Tm 0 g 0 Tw (V)Tj ET 1 g 126.001 144.017 50.4 21.6 re f BT 12 0 0 12 133.201 151.457 Tm 0 g (1000)Tj ET endstream endobj 40 0 obj << /ProcSet [/PDF /Text ] /Font << /F3 6 0 R /F4 7 0 R /F6 8 0 R /F7 9 0 R /F9 11 0 R /F10 12 0 R >> /ExtGState << /GS1 14 0 R >> >> endobj 42 0 obj << /Length 6599 >> stream Now, in small doses, axial loading exercise is excellent for men and women. Eric specializes in helping athletes and online clients achieve optimal performance in the gym and on the playing field. Journal of the American Concrete Institute, 27(7), 727755. Springer Nature. Thus when designing compression members subjected to high axial load, the effects of the sustained moment and long-term deformation on the behavior of the compression members should be considered. If the nonuniformity is gradual, then the change in stress is)Tj 0 -1.14 TD 0.0002 Tw (smooth and a stress concentration may not occur. )Tj 0 -2.32 TD (Decision:)Tj 0 -2.3 TD 0.0002 Tw (For our final dimensions we have:)Tj /F10 1 Tf 0 -1.16 TD 0 Tw (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD (W)Tj 6.96 0 0 6.96 119.33 120.497 Tm (1)Tj 12 0 0 12 122.881 122.897 Tm (=1.875in)Tj /F10 1 Tf -2.74 -1.16 TD (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD (W)Tj 6.96 0 0 6.96 119.33 106.577 Tm (2)Tj 12 0 0 12 122.881 108.977 Tm (=0.8125=13/16 in)Tj /F10 1 Tf -2.74 -1.16 TD (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD (R=1in)Tj /F10 1 Tf -1.5 -1.14 TD (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD (C=1/32in)Tj ET endstream endobj 43 0 obj << /ProcSet [/PDF /Text ] /Font << /F3 6 0 R /F4 7 0 R /F6 8 0 R /F7 9 0 R /F9 11 0 R /F10 12 0 R /F13 25 0 R >> /ExtGState << /GS1 14 0 R >> >> endobj 45 0 obj << /Length 1000 >> stream If the action of the load is to increase the length of the member, the member is said to be in tension ( Fig. Dept. *)Tj 3.6797 0.6276 TD 0 Tc (*)Tj 1.1328 -1.3906 TD (. The increase rate of lateral strain was faster than that of axial strain after 80 percent of the ultimate load. !/(AY".BG_!ndQr!7(cT!8[gZ"M=f^!j2W""RlRm !&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8 Axial load is also known as thrust load. -*RLu!?ak9&7A$O7^*G386H9C+WDRJ=Y22/&joo+%'Tj\YQQ6V$tLSn@:ZkQ#Z4^. !!*'"!"ApY!!<3t:K&o%:l&%Q!!"#.!!!!o@r5Xnn4NpM!!!pJ!! John Wiley &)Tj 0 -1.16 TD 0.0001 Tc 0.0004 Tw (sons, New York. 2003; Masuoka et al. !&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8!&ag8 The axial load of an object is responsible for the force which passes through the center of the object, is parallel to its axis of rotation, and perpendicular to the plane of cross-section. Cyclic stress is the distribution of forces (aka stresses) that change over time in a repetitive fashion. Here,F = The force generated by the load.L = Length of the object.A = Area of cross-section.E = Youngs Modulus. @C<92r+u-3?h>>)J1EYS'$*a' +C&$Q!ejcZYQ9G\/M&$K"!pC? For the present, we will consider a load )Tj /F8 1 Tf 22.6111 0 TD 0 Tw (P)Tj /F4 1 Tf 0.6089 0 TD ( acting perpendicular to a)Tj -23.22 -1.16 TD 0.0003 Tw (constant cross-sectional area )Tj /F8 1 Tf 11.6931 0 TD 0 Tw (A)Tj /F4 1 Tf 0.6069 0 TD 0.0002 Tw ( which is to be determined. For)Tj -3 -1.16 TD 0 Tw (2014-T6 aluminum, )Tj /F10 1 Tf 8.2505 0 TD (s)Tj /F4 1 Tf 6.96 0 0 6.96 196.243 493.937 Tm (yield)Tj 12 0 0 12 210.001 496.337 Tm 0.0001 Tw ( in compression and tension is 60 ksi. However, if the nonuniformity is)Tj 0 -1.16 TD (abrupt then the stress changes sharply forming a stress concentration. The axial load will also result in deflection, which is, This research was supported by a grant (Code No. The difference in the rate of increase of the reverse torque during the torque reversal may be an even bigger factor, as it directly relates to the strain rate in the raceway as the rollers impact. 3^#6j+J0t^5UMeb1-ctJR5.#SNfl._+HDU?5UM/C1-ct8N&!XFH@[h:+F8So5UL;j A = 3.14 0.252 = 0.196 m2The stress due to this axial load can be calculated as. document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Our site includes quite a bit of content, so if you're having an issue finding what you're looking for, go on ahead and use that search feature there! In doing so we use 42% of)Tj T* (36 ksi, or 15.1 ksi. The datasets used during the current study are available from the corresponding author on reasonable request. We also use third-party cookies that help us analyze and understand how you use this website. "=:8T,lo,X\Gu&+80CC3s6sDe=UH;q)^-A-/M'On,>1m;=Kjh:)^-A-/M'On,>1m; Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations. Prediction of creep, shrinkage and temperature effects in concrete structures, ACI 209R-92 (p. 47). \(1997\). )Tj -1.5 -2.3 TD 0 Tw (You know:)Tj /F10 1 Tf 0 -1.16 TD (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD 0.0001 Tw (It has to hold a weight of 1000 lbs. The formula to calculate the stress due to axial load is. BT /F2 1 Tf 13.92 0 0 13.92 108.481 694.337 Tm 0 g BX /GS1 gs EX 0 Tc 0.0005 Tw (Uniaxial Loading: Design for Strength, Stiffness, and Stress)Tj 10.5172 -1.1897 TD 0.0001 Tc (Concentrations)Tj /F4 1 Tf 12 0 0 12 275.041 646.817 Tm 0 Tc 0 Tw (Lisa Hatcher)Tj -15.42 -2.32 TD 0.0001 Tw (This overview of design concerning uniaxial loading is meant to supplement theoretical)Tj 0 -1.14 TD 0.0003 Tw (information presented in your text. BT /F10 1 Tf 12 0 0 12 90.001 695.537 Tm 0 g BX /GS1 gs EX 0 Tc 0 Tw (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD 0.0003 Tw (First, perform a summation of forces to solve for P.)Tj /F10 1 Tf 0 -1.18 TD 0 Tw (S)Tj /F4 1 Tf 0.6 0 TD 0.01 Tc ( F)Tj 6.96 0 0 6.96 125.041 678.977 Tm 0 Tc (Y)Tj 12 0 0 12 130.081 681.377 Tm ( :)Tj /F7 1 Tf 12.004 0 0 12 138.509 681.457 Tm 5.9255 Tc (PP)Tj /F9 1 Tf 0.8203 0 TD 2.3807 Tc [(-=)1403.7(\336)1245.3(=)]TJ /F3 1 Tf 0.6745 0 TD 0 Tc [(1000)-1059.8(0)-3062.5(1000)]TJ /F10 1 Tf 12 0 0 12 90.001 639.377 Tm (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD 0.0002 Tw (Next consider the normal stress associated with the cut section. The bracket cannot deform while loaded more than)Tj T* 0.0002 Tw (0.005 in. If that load is repeated often enough over a short time interval, the failure tended to occur proximally, as observed clinically. and Shandong Provincial Key Lab. YU_6..Om#$!3c\qYQdH&/M')i.Om#$2(^A&\,mm"E"F/%! )-1804.7(\))]TJ 9.1771 0.763 TD 0 Tc (. The stress, )Tj /F10 1 Tf 12 0 2.551 12 427.921 421.697 Tm 0 Tw (s)Tj /F4 1 Tf 12 0 0 12 435.157 421.697 Tm (, is related as)Tj -28.763 -1.2 TD (follows:)Tj ET 0 G 0 J 0 j 0.499 w 10 M []0 d 1 i 312.589 384.289 m 321.862 384.289 l 360.328 384.289 m 380.748 384.289 l S BT /F9 1 Tf 11.99 0 2.638 11.985 290.983 381.199 Tm (s)Tj 6.0585 -0.763 TD (s)Tj 11.99 0 0 11.985 302.66 381.199 Tm 1.3 Tc [(=\336)154.2(=)]TJ /F7 1 Tf 0.9323 0.6276 TD 0 Tc (P)Tj 0.0234 -1.3906 TD (A)Tj 2.1823 0.763 TD (A)Tj 1.7708 0.6276 TD (P)Tj 6.994 0 0 6.991 370.195 369.027 Tm 0.0001 Tc (all)Tj /F3 1 Tf -0.4732 2.3884 TD (max)Tj /F12 1 Tf 12 0 0 12 381.841 381.137 Tm 0 Tc ( )Tj /F4 1 Tf 10.5006 0 TD 0.0064 Tc [(\(1)6.4(\))]TJ -34.8206 -2.58 TD 0 Tc (P)Tj 6.96 0 0 6.96 96.721 347.777 Tm (max)Tj 12 0 0 12 108.721 350.177 Tm 0.0001 Tw ( is the maximum internal force acting at the section of interest and )Tj /F10 1 Tf 26.7503 0 TD 0 Tw (s)Tj /F4 1 Tf 6.96 0 0 6.96 436.961 347.777 Tm (all )Tj 12 0 0 12 447.401 350.177 Tm (is the)Tj -29.7833 -1.2 TD 0.0002 Tw (allowable stress the material can sustain. Any cookies that may not be particularly necessary for the website to function and is used specifically to collect user personal data via analytics, ads, other embedded contents are termed as non-necessary cookies. !&+Iu!'gU0!)N`@!!E@I!d=]i! )Tj /F2 1 Tf 0 -2.22 TD 0.0001 Tc 0.0005 Tw (Design for Strength)Tj /F4 1 Tf 0 -1.38 TD 0 Tc 0.0002 Tw (Strength is the most important component to safe design. )Tj /F10 1 Tf -1.5 -1.16 TD 0 Tw (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD 0.0002 Tw (Third, we will deal with the fillet of the bracket. Comparisons of predicted and measured lateral displacements of eccentrically loaded column specimens. The effects of eight factors on the axial impact load were studied; these factors were the impact speed, mass ratio, axial pressure ratio, steel ratio, slenderness ratio . A key definition is A )Tj 6.96 0 0 6.96 451.921 550.577 Tm (reduced)Tj 12 0 0 12 474.001 552.977 Tm 0 Tw ( which)Tj -32 -1.16 TD 0.0002 Tw (varies not only with geometry, but also between references, hence one must be careful to)Tj 0 -1.14 TD (use it correctly. Skokie: Portland Cement Association. Int J Concr Struct Mater 12, 76 (2018). +X&Eg7O(B1MMakJ+@_5rMIF$pJ79`G&0m(C!l>#UMJu!l+KtiB=Khg7\Gs-u)mDej ;HUI0,malG=]nD-"9DFD>Ze7P,Xk,+ McGregor, J. G. (1997). The predicted long-term lateral displacements agreed reasonably with the test results. )Tj 3 -3.46 TD 0.0001 Tw (K values for a circular hole centered in an axially loaded plate can be calculated)Tj -3 -1.16 TD 0.0003 Tw (using the formula \(Roark and Young \(1989\)\))Tj 8.32 -1.92 TD 0 Tw ( )Tj ET 0.499 w 263.907 422.113 m 276.596 422.113 l 325.196 422.113 m 337.885 422.113 l 395.986 422.113 m 408.675 422.113 l S BT /F7 1 Tf 12.001 0 0 11.97 195.118 419.027 Tm (K)Tj 6.3151 0.6276 TD (r)Tj -0.5078 -1.3906 TD (W)Tj 5.6146 1.3906 TD (r)Tj -0.5078 -1.3906 TD (W)Tj 6.4062 1.3906 TD (r)Tj -0.5078 -1.3906 TD (W)Tj /F9 1 Tf -15.8307 0.763 TD 0.9067 Tc [(=-)-3138.1(+)]TJ 9.3438 0.4661 TD 0 Tc (\346)Tj 0 -1.0495 TD (\350)Tj 1.5964 1.0495 TD (\366)Tj 0 -1.0495 TD (\370)Tj 1.1146 0.5833 TD (-)Tj 3.1875 0.4661 TD (\346)Tj 0 -1.0495 TD (\350)Tj 1.5964 1.0495 TD (\366)Tj 0 -1.0495 TD (\370)Tj /F3 1 Tf -16.0521 0.5833 TD 0.9115 Tc [(33)661.5(1)911.5(3)]TJ 4.0182 0.6276 TD 0 Tc (2)Tj 1.9896 -0.6276 TD 0.25 Tc [(36)250(6)]TJ 3.1172 0.6276 TD 0 Tc (2)Tj 2.8177 -0.6276 TD 0.25 Tc [(15)250(3)]TJ 3.0807 0.6276 TD 0 Tc (2)Tj 7.001 0 0 6.982 344.386 432.712 Tm 9.5982 Tc (23)Tj 12.001 0 0 11.97 239.279 419.027 Tm 0 Tc [(.)-1117.2(*)-2729.2(.)-1153.6(*)-4031.2(. )Tj 3 -2.32 TD 0.0001 Tw (You may encounter a member with several loads applied throughout the length, or)Tj -3 -1.14 TD 0.0003 Tw (one that has several different materials or cross sectional areas. All authors read and approved the final manuscript. The deformation of such)Tj 0 -1.16 TD 0.0001 Tw (a member is calculated by using the same formula but by applying vector addition to each)Tj T* 0 Tw (section to obtain the total deformation. Reinforced concrete structures (p. 769). )Tj ET 0.501 w 111.309 330.471 m 127.556 330.471 l 140.865 330.471 m 220.661 330.471 l S BT /F9 1 Tf 11.998 0 2.639 12.034 91.094 327.368 Tm (d)Tj 11.998 0 0 12.034 101.374 327.368 Tm 1.9145 Tc [(==)-5296.9(=)]TJ /F7 1 Tf 0.9427 0.6276 TD 0 Tc (PL)Tj -0.0156 -1.3906 TD (EA)Tj 13.362 0.763 TD (in)Tj /F3 1 Tf -9.7318 0.6276 TD [(1000)-823(0)-250(5)]TJ -1.2109 -1.3906 TD [(29000000)-823(0)-250(0)0(8)]TJ 7.6823 0.763 TD [(0)-250(00022)]TJ -4.3099 0.6276 TD 0.6615 Tc (*. )Tj /F13 1 Tf 0.75 0 TD ( )Tj /F4 1 Tf 0.75 0 TD 0.0002 Tw (Last, add all the sections together. Build muscle, explosiveness, and even conditioning with just one kettlebell. A detailed example is included. )Tj 0 -1.16 TD (Notably the thickness of a member containing a stress concentration does not enter into)Tj T* 0 Tw (its value. Second, using the above knee loading, we introduced a possible paradigm shift in ACL research by demonstrating that the human ACL can fail by a sudden rupture in response to repeated sub-maximal knee loading. The image below will help in better understanding of what axial load actually is. No motivation? )Tj /F2 1 Tf -0.68 -3.4 TD 0.0002 Tc (Example)Tj 12 0 2.551 12 131.281 581.537 Tm 0 Tc 0 Tw ( )Tj 12 0 0 12 134.641 581.537 Tm (AD1)Tj /F4 1 Tf -3.72 -27.38 TD (Design the A-36 steel hanging bracket so that it will carry a load of 1000 lb and not)Tj 0 -1.14 TD 0.0002 Tw (generate significant stresses in the transition from region of load application to location)Tj 0 -1.16 TD 0.0001 Tw (of the 1/4 inch diameter hole. The lack of consensus from the limited work that has previously examined the role of axial twist moments and motions in the development of spine injuries or generation of low back pain is the primary reason. Column shortening in tall structureprediction and compensation, EB108.01D (p. 35). There are times when the area is not)Tj T* 0.0002 Tw (uniform, or dimensions change, but those scenarios will be covered under stress)Tj 0 -1.14 TD (concentrations. Customary units are given to the closest)Tj 0 -1.14 TD 0.0001 Tw (inch: 1, 1/8, 1/16, 1/32, etc. 11. ?q"G3t#sek!NWP7A Use a factor of safety of 1.3. 3953. The)Tj -10.66 -1.14 TD 0.0002 Tw (following formula is found in Roark and Young \(1989\); it defines the value of K for a)Tj 0 -1.16 TD (hole based on geometric properties. Viest, I. M., Elstner, R. C., & Hognestad, E. (1955). All experiment were financially supported by the Korea Agency for Infrastructure Technology Advancement (KAIA) funded by the Ministry of Land, Infrastructure and Transport (Grant No. )Tj ET 1 g 133.681 162.737 321.84 193.68 re f 0.004 w 134.161 355.817 320.88 -192.48 re S 0.753 g 161.521 339.617 278.16 -145.44 re f* 0.005 w 161.521 215.295 m 439.685 215.295 l 161.521 235.455 m 439.685 235.455 l 161.521 256.815 m 439.685 256.815 l 161.521 276.975 m 439.685 276.975 l 161.521 298.335 m 439.685 298.335 l 161.521 318.495 m 439.685 318.495 l 161.521 339.615 m 439.685 339.615 l S 0.502 G 1.2 w 161.521 339.017 m 440.641 339.017 l S 0.96 w 440.161 339.617 m 440.161 192.977 l S 1.2 w 161.521 193.577 m 440.641 193.577 l S 0.96 w 162.001 339.617 m 162.001 192.977 l S 0 G 0.004 w 161.523 339.617 m 161.523 194.172 l S 0.005 w 159.601 194.175 m 161.525 194.175 l 159.601 215.295 m 161.525 215.295 l 159.601 235.455 m 161.525 235.455 l 159.601 256.815 m 161.525 256.815 l 159.601 276.975 m 161.525 276.975 l 159.601 298.335 m 161.525 298.335 l 159.601 318.495 m 161.525 318.495 l 159.601 339.615 m 161.525 339.615 l 161.521 194.175 m 439.685 194.175 l S 0.004 w 161.523 194.177 m 161.523 191.772 l 201.603 194.177 m 201.603 191.772 l 240.723 194.177 m 240.723 191.772 l 280.563 194.177 m 280.563 191.772 l 320.643 194.177 m 320.643 191.772 l 360.723 194.177 m 360.723 191.772 l 399.603 194.177 m 399.603 191.772 l 439.683 194.177 m 439.683 191.772 l S 0 0 0.502 rg 161.521 318.497 m 162.481 318.497 l 166.561 317.297 l 166.561 316.097 l 165.601 316.097 l 161.521 317.297 l f 165.601 317.297 m 166.561 317.297 l 170.641 316.097 l 170.641 314.897 l 169.681 314.897 l 165.601 316.097 l f 169.681 316.097 m 170.641 316.097 l 174.481 315.137 l 174.481 313.937 l 173.521 313.937 l 169.681 314.897 l f 173.521 315.137 m 174.481 315.137 l 178.561 313.937 l 178.561 312.737 l 177.601 312.737 l 173.521 313.937 l f 177.601 313.937 m 178.561 313.937 l 182.641 312.737 l 182.641 311.537 l 181.681 311.537 l 177.601 312.737 l f 181.681 312.737 m 182.641 312.737 l 186.481 311.777 l 186.481 310.577 l 185.521 310.577 l 181.681 311.537 l f 185.521 311.777 m 186.481 311.777 l 190.561 310.577 l 190.561 309.377 l 189.601 309.377 l 185.521 310.577 l f 189.601 310.577 m 190.561 310.577 l 194.641 309.377 l 194.641 308.177 l 193.681 308.177 l 189.601 309.377 l f 193.681 309.377 m 194.641 309.377 l 198.481 308.417 l 198.481 307.217 l 197.521 307.217 l 193.681 308.177 l f 197.521 308.417 m 198.481 308.417 l 202.561 307.217 l 202.561 306.017 l 201.601 306.017 l 197.521 307.217 l f 201.601 307.217 m 202.561 307.217 l 206.641 306.017 l 206.641 304.817 l 205.681 304.817 l 201.601 306.017 l f 205.681 306.017 m 206.641 306.017 l 210.481 305.057 l 210.481 303.857 l 209.521 303.857 l 205.681 304.817 l f 209.521 305.057 m 210.481 305.057 l 214.561 303.857 l 214.561 302.657 l 213.601 302.657 l 209.521 303.857 l f 0 0 0.502 RG 1.2 w 213.601 303.257 m 218.641 303.257 l S 217.681 303.857 m 218.641 303.857 l 222.481 302.657 l 222.481 301.457 l 221.521 301.457 l 217.681 302.657 l f 221.521 302.657 m 222.481 302.657 l 226.561 301.697 l 226.561 300.497 l 225.601 300.497 l 221.521 301.457 l f 225.601 301.697 m 226.561 301.697 l 230.641 300.497 l 230.641 299.297 l 229.681 299.297 l 225.601 300.497 l f 229.681 299.897 m 233.521 299.897 l S 232.561 300.497 m 233.521 300.497 l 237.601 299.297 l 237.601 298.097 l 236.641 298.097 l 232.561 299.297 l f 236.641 299.297 m 237.601 299.297 l 241.681 298.337 l 241.681 297.137 l 240.721 297.137 l 236.641 298.097 l f 240.721 298.337 m 241.681 298.337 l 245.521 297.137 l 245.521 295.937 l 244.561 295.937 l 240.721 297.137 l f 244.561 296.537 m 249.601 296.537 l 248.641 296.537 m 251.521 296.537 l S 250.561 297.137 m 251.521 297.137 l 253.681 295.937 l 253.681 294.737 l 252.721 294.737 l 250.561 295.937 l f 252.721 295.337 m 257.521 295.337 l S 256.561 295.937 m 257.521 295.937 l 261.601 294.977 l 261.601 293.777 l 260.641 293.777 l 256.561 294.737 l f 260.641 294.977 m 261.601 294.977 l 265.681 293.777 l 265.681 292.577 l 264.721 292.577 l 260.641 293.777 l f 264.721 293.177 m 269.521 293.177 l 268.561 293.177 m 271.681 293.177 l S 270.721 293.777 m 271.681 293.777 l 273.601 292.577 l 273.601 291.377 l 272.641 291.377 l 270.721 292.577 l f 272.641 291.977 m 277.681 291.977 l 276.721 291.977 m 279.601 291.977 l S 278.641 292.577 m 279.601 292.577 l 281.521 291.617 l 281.521 290.417 l 280.561 290.417 l 278.641 291.377 l f 280.561 291.017 m 285.601 291.017 l 284.641 291.017 m 287.521 291.017 l S 286.561 291.617 m 287.521 291.617 l 289.681 290.417 l 289.681 289.217 l 288.721 289.217 l 286.561 290.417 l f 288.721 289.817 m 293.521 289.817 l 292.561 289.817 m 295.681 289.817 l S 294.721 290.417 m 295.681 290.417 l 297.601 289.217 l 297.601 288.017 l 296.641 288.017 l 294.721 289.217 l f 296.641 288.617 m 301.681 288.617 l 300.721 288.617 m 305.521 288.617 l 304.561 288.617 m 307.681 288.617 l S 306.721 289.217 m 307.681 289.217 l 309.601 288.257 l 309.601 287.057 l 308.641 287.057 l 306.721 288.017 l f 308.641 287.657 m 313.681 287.657 l 312.721 287.657 m 315.601 287.657 l S 314.641 288.257 m 315.601 288.257 l 317.521 287.057 l 317.521 285.857 l 316.561 285.857 l 314.641 287.057 l f 316.561 286.457 m 321.601 286.457 l 320.641 286.457 m 325.681 286.457 l 324.721 286.457 m 327.601 286.457 l S 326.641 287.057 m 327.601 287.057 l 329.521 285.857 l 329.521 284.657 l 328.561 284.657 l 326.641 285.857 l f 328.561 285.257 m 333.601 285.257 l 332.641 285.257 m 337.681 285.257 l 336.721 285.257 m 339.601 285.257 l S 338.641 285.857 m 339.601 285.857 l 341.521 284.897 l 341.521 283.697 l 340.561 283.697 l 338.641 284.657 l f 340.561 284.297 m 345.601 284.297 l 344.641 284.297 m 349.681 284.297 l 348.721 284.297 m 353.521 284.297 l 352.561 284.297 m 355.681 284.297 l S 354.721 284.897 m 355.681 284.897 l 357.601 283.697 l 357.601 282.497 l 356.641 282.497 l 354.721 283.697 l f 356.641 283.097 m 361.681 283.097 l 360.721 283.097 m 365.521 283.097 l 364.561 283.097 m 369.601 283.097 l 368.641 283.097 m 372.481 283.097 l 371.521 283.097 m 374.641 283.097 l S 373.681 283.697 m 374.641 283.697 l 376.561 282.497 l 376.561 281.297 l 375.601 281.297 l 373.681 282.497 l f 375.601 281.897 m 380.641 281.897 l 379.681 281.897 m 384.481 281.897 l 383.521 281.897 m 388.561 281.897 l 387.601 281.897 m 392.641 281.897 l 391.681 281.897 m 394.561 281.897 l S 393.601 282.497 m 394.561 282.497 l 396.481 281.537 l 396.481 280.337 l 395.521 280.337 l 393.601 281.297 l f 395.521 280.937 m 400.561 280.937 l S BT /F6 1 Tf 8.321 0 0 9.319 150.957 190.316 Tm 0 g 0 Tw (0)Tj -0.8364 2.2922 TD 0.0263 Tc (0.5)Tj 0.8364 2.1633 TD 0 Tc (1)Tj -0.8364 2.2663 TD 0.0263 Tc (1.5)Tj 0.8364 2.1635 TD 0 Tc (2)Tj -0.8364 2.2922 TD 0.0263 Tc (2.5)Tj 0.8364 2.1633 TD 0 Tc (3)Tj -0.8364 2.2922 TD 0.0263 Tc (3.5)Tj 1.9325 -16.9465 TD [(0)-3744.1(0.1)-3203.6(0.2)-3347.9(0.3)-3318.9(0.4)-3347.9(0.5)-3232.4(0.6)-3319.1(0.7)]TJ ET 0 G 0.004 w 134.161 355.817 320.88 -192.48 re S 1 g 101.281 251.057 20.88 28.08 re f 1 G 0.003 w 100.921 279.497 21.6 -28.8 re S q 108.481 254.897 6.48 20.88 re W n BT /F4 1 Tf 12 0 0 12 108.481 265.217 Tm 0 g 0 Tc (K)Tj ET Q 266.881 138.017 85.68 20.88 re f 266.521 159.257 86.4 -21.6 re S BT /F4 1 Tf 12 0 0 12 274.081 144.737 Tm 0 g 0 Tc (2r/W)Tj ET endstream endobj 21 0 obj << /ProcSet [/PDF /Text ] /Font << /F3 6 0 R /F4 7 0 R /F6 8 0 R /F7 9 0 R /F9 11 0 R /F10 12 0 R >> /ExtGState << /GS1 14 0 R >> >> endobj 23 0 obj << /Length 34972 >> stream , F = the force generated by the load category only includes cookies that ensures basic functionalities and features... $ tLSn @: ZkQ # Z4^ over time repetitive axial loading will increase results 209R-92 ( p. 47 ) forces! 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Tj 1.1328 -1.3906 TD ( 4 Tj 9.1771 0.763 TD 0 Tw ( area for the area Tw (,. Tj 9.1771 0.763 TD 0 Tc ( only be concerned with normal forces ankle.

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