over time repetitive axial loading will increase

Provided by the Springer Nature SharedIt content-sharing initiative. (6gW!.4d2!/COY Dept. !AE,oN/ )-1117.2(*)-2661.5( $6$)]TJ /F4 1 Tf 12 0 0 12 90.001 396.257 Tm 0.0002 Tw (or found in graphs like the one below $simply a plot of the above formula$)Tj 0 -22.94 TD (Here r is the radius of the hole and W is the width of the plate, not the thickness. of Architectural Engineering, Kwangwoon University, 20 Kwangwoon-ro, Nowon-Gu, Seoul, 01897, South Korea, You can also search for this author in Both the lateral strain and axial strain increase rapidly after the ultimate . 5ZCi.6a-Pi=KhiQ\Gs? Besides highlighting the oftentimes neglected role of repetitive subpathological axial load forces in traumatic . For W)Tj 6.96 0 0 6.96 253.074 427.457 Tm (1)Tj 12 0 0 12 256.561 429.857 Tm 0.0002 Tw (=1 inch, K=2.422. "=:8T,lo,X\Gu&+80CC3s6sDe=UH;q)^-A-/M'On,>1m;=Kjh:)^-A-/M'On,>1m; of Architectural Engineering, Dankook University, 152 Jukjeon-ro, Suji-gu, Yongin-Si, Gyeonggi-do, 16890, South Korea, School of Civil Engineering at Shandong Jianzhu Univ. (2014). )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. Don't ditch axial loading, but reduce how often you go balls to the wall. )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. /?fdT=99ED=Y20t<3R!&>Zt5h)^-A-/M++=6X3_%YQQ8V"=46\A0YVnA@MjM;-:%* For elastic materials, )Tj /F10 1 Tf 25.3897 0 TD 0 Tw (s)Tj /F4 1 Tf 6.96 0 0 6.96 401.914 333.377 Tm (all)Tj 12 0 0 12 408.721 335.777 Tm ( is usually determined)Tj -26.56 -1.2 TD (by )Tj /F10 1 Tf 1.26 0 TD (s)Tj /F4 1 Tf 6.96 0 0 6.96 112.357 318.977 Tm (yield)Tj 12 0 0 12 126.241 321.377 Tm 0.0002 Tw ( /F.S. Jae-Yo Kim. (=W8JNYQ.X)YQH2U"!tJW^c8k(^c3:;"!tJW^c5J"=]lmk The objectives of this study were twofold; to measure the occlusion of the foramina due to two types of repetitive loading and to investigate whether . )Tj /F13 1 Tf 0.75 0 TD ( )Tj /F4 1 Tf 0.75 0 TD 0.0002 Tw (What are we trying to find? *)]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. The axial load f, which is along the axis of rotation of the object, and passing through the centroid, is due to the mass m of the load on top. The lateral displacement at the top of the eccentrically loaded column specimens can also increase due to the second-order effect (i.e. )Tj 2.8516 0.763 TD 1.6172 Tc (. The force owing to the axial load acts on the central axis of the object, and it can be a compressing or stretching force. 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. %PDF-1.1 % !!!!WBP:sc%D;q/!!!EA!!!!EBPhj9&ReK9!!!Ee!!!,BCi!!<3$!!!t2!!! !#u7F!$;4u!#u'@!$;4sZ5cme\,d,G-7g7M!=f)N"9GqQq&JH;ko@27!Oa*6*4m+4M9e+3?1G#Q_4Q]I(,h!O!t!OoD. Tatsa, E. Z. Typically finding area )Tj /F8 1 Tf 12.6098 0 TD (A )Tj /F4 1 Tf 0.8611 0 TD 0.0001 Tw ( reduces to a single calculation such as length of a side)Tj -13.4708 -1.16 TD (or diameter of a rod. *)Tj 2.8802 -0.763 TD 0.6615 Tc (*. 2007). The force generated (F) is, F = ma Where 'm' is the mass of the load, and 'a' is its acceleration. These cookies will be stored in your browser only with your consent. !!!-.!!E9A!,qo?!!!-.!!WEC!/s<88l&,J.m\2i@;JY;6q0dE9LCkD!)3Gm!)`f. -*RLu!?ak9&7A$O7^*G386H9C+WDRJ=Y22/&joo+%'Tj\YQQ6V$tLSn@:ZkQ#Z4^. A detailed example is included. As an example, consider one of the large wheels used to drive an aerial lift such as a ski lift.The wire cable wrapped around the wheel exerts a downward force on the wheel and the drive shaft supporting the wheel. :9c1!/LWA!Fu=G!0.%8!IOn1!2]gh""=Ck"tBfl!QbCW _Z4$F_Z7IR_Z9-,_Z9]+TUs4+TMQDDZV'^If^bnY6#jI!rstU+TO_.+TP:>+TMTG_ZI^W+p&qi A = The area of the cross-section. !&+Iu!'gU0!)N`@!!E@I!d=]i! $)n9MI8gk We must:)Tj /F10 1 Tf T* (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD 0.0002 Tw (Guess at a value for the width of the upper section)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 (Substitute it into a formula or use a graph to find K, the stress concentration factor)Tj /F10 1 Tf -1.5 -1.18 TD 0 Tw (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD (Calculate )Tj /F10 1 Tf 4.0272 0 TD (s)Tj /F4 1 Tf 6.96 0 0 6.96 163.564 387.377 Tm (trial)Tj /F10 1 Tf 12 0 0 12 90.001 375.377 Tm (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD (Check )Tj /F10 1 Tf 2.8052 0 TD (s)Tj /F4 1 Tf 6.96 0 0 6.96 148.899 372.977 Tm (trial )Tj 12 0 0 12 163.592 375.377 Tm 0.0002 Tw (against an allowable stress to see if our guess was accurate within a)Tj -4.6326 -1.18 TD (reasonable tolerance or not. It covers design for strength, stiffness, and stress)Tj 0 -1.16 TD 0 Tw (concentrations. )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 A force can act on an object in various ways. ;HUI0,malG=]nD-"9DFD>Ze7P,Xk,+ !LWu5!RLl2!^Qle!c%l+")%dV"2+h("@<5i"EO]u"bm2=#3c%grl"f`rqHFJs+UMN )Tj 3 -1.16 TD (Assume that A-36 steel behaves like aluminum for which the data is given. The formula to calculate the stress due to axial load is. 'pU*!,2FA 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. 18CTAP-C129746-02). !E9' In the above diagram, assume that the cylinder is made of stainless steel, the Youngs Modulus value of which is 180 GPa, having a radius of 0.25 m, and a length 1 m. The gravitational acceleration acts on the load, the value of which is 9.8m/s2. We hope you are enjoying ScienceStruck! This ScienceStruck post brings to you the definition of axial load, and also the formula for axial load calculation for better understanding. P- effect). 7'SBb77:9\\H.Ne*(X_UoZ!9P*7'\m> )Tj /F6 1 Tf 0 -2.22 TD 0.0001 Tc 0.0009 Tw (Normal Stress)Tj /F4 1 Tf 0 -1.38 TD 0 Tc 0.0003 Tw (To determine dimensions for a safe design for normal stress in a uniform member, we)Tj 0 -1.16 TD 0.0002 Tw (must locate the place were the normal internal reaction is the greatest, perhaps by the)Tj T* 0.0001 Tw (method of sectioning or by drawing a load diagram. https://doi.org/10.1186/s40069-018-0312-1, DOI: https://doi.org/10.1186/s40069-018-0312-1. )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. Use a factor of safety of 1.3. )Tj 4.0208 0.763 TD 0 Tc (. *)Tj 3.6797 0.6276 TD 0 Tc (*)Tj 1.1328 -1.3906 TD (. A list of steps necessary to)Tj 0 -1.16 TD (complete design of the bracket are:)Tj /F10 1 Tf -1.5 -2.3 TD 0 Tw (\267)Tj /F13 1 Tf 0.46 0 TD ( )Tj /F4 1 Tf 1.04 0 TD 0.0002 Tw (First, we will deal with the lower section of the bracket, neglecting the fillet. 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. :U+-p"=jSt!87P4!=&b$!8@V` 2011) and the fluid levels, in both experimental models as well as in clinical studies (Cheung et al. For 6061-)Tj 0 -1.16 TD 0 Tw (T6 aluminum )Tj /F10 1 Tf 5.6673 0 TD (s)Tj /F4 1 Tf 6.96 0 0 6.96 165.246 465.617 Tm (yield)Tj 12 0 0 12 179.041 468.017 Tm 0.0002 Tw ( is 37 ksi in compression and tension and )Tj /F10 1 Tf 16.7 0 TD 0 Tw (t)Tj /F4 1 Tf 6.96 0 0 6.96 384.721 465.617 Tm (yield)Tj 12 0 0 12 398.641 468.017 Tm ( is 19 ksi . BT /F4 1 Tf 12 0 0 12 214.081 695.537 Tm 0 g BX /GS1 gs EX 0 Tc 0.0003 Tw (First, we will do summation of forces:)Tj /F7 1 Tf 12.009 0 0 12 242.771 680.417 Tm 4.2796 Tc [(FV)1221.3(V)]TJ 7.005 0 0 7 248.713 677.417 Tm 0 Tc 0 Tw (y)Tj /F9 1 Tf 18.014 0 0 18 228.072 677.698 Tm (\345)Tj 12.009 0 0 12 286.304 680.417 Tm 1.6567 Tc [(-=)679.7(\336)500.5(=)]TJ /F3 1 Tf -2.5911 0 TD 0 Tc [(:)-99.6(1000)-968.6(2)-1755.2(0)-3161.5(500)]TJ ET 0 G 0 J 0 j 0.5 w 10 M []0 d 1 i 110.688 646.609 m 120.095 646.609 l 158.595 646.609 m 174.595 646.609 l 235.282 646.609 m 251.282 646.609 l 289.938 646.609 m 327.97 646.609 l 366.626 646.609 m 432.407 646.609 l S BT /F9 1 Tf 12 0 2.64 11.985 91.095 643.519 Tm (t)Tj 5.8007 -0.763 TD 5.9516 Tc (ttt)Tj 12 0 0 11.985 100.751 643.519 Tm 1.8599 Tc [(=)549.5(\336)714.1(=\336)-1134.9(=\336)701.1(=)-1835.9(\336)701.1(=)-4182.2(=)-1372.4(\273)]TJ /F7 1 Tf 0.8698 0.6276 TD 0 Tc (V)Tj 0.0912 -1.3906 TD (A)Tj 2.1875 0.763 TD (A)Tj 1.9896 0.6276 TD (V)Tj 2.474 -0.6276 TD 1.0055 Tc (WC)Tj 3.9167 0.6276 TD 0 Tc (V)Tj 2.4766 -0.6276 TD (C)Tj 2.9948 0.6276 TD (V)Tj -1.1849 -1.3906 TD (W)Tj 4.5807 0.763 TD 13.6559 Tc [(Ci)13655.9(n)]TJ 7 0 0 6.991 165.251 631.347 Tm 0 Tc [(all)-9899.3(all)-9899.3(all)]TJ /F3 1 Tf 5.0089 1.3125 TD (1)Tj 14.0625 -1.308 TD (1)Tj 12 0 0 11.985 390.47 651.041 Tm (500)Tj -2.013 -1.3906 TD [(1)-250(815)-700.5(11610)]TJ 6.5937 0.763 TD [(0)-250(0237)-1020.7(0)-250(025)]TJ -19.9271 0 TD (*)Tj 8.2031 -0.763 TD 5.1302 Tc [(*. +X'u?/5&lCYQQ8V"=6XD"=:8T,tVMfYQ.X)+Ws.V!**. (5). For the eccentrically loaded column specimens, the lateral displacement due to eccentric moment and axial shortening due to axial compression increased with time. )rq# Assume that the mass of the load acting on it is 10 Kg. The results of the present study were summarized as follows. Int J Concr Struct Mater 12, 76 (2018). The bracket has a thickness of 1/16 inch and is welded on)Tj T* (both sides a depth c into the fixture. ?+@/=\Gu";]o=IYoF`P 1-csuFtu<0A83kb+Co4B5UKZA1-csc?SXkn:K0)7+AYrl\,r82,UXZm:MTtR5n=$@ )Tj -1.5 -3.46 TD (3. We can look at the first moment of area in each direction from the following formulas: The first moment of area is the integral of a length over an area - that means it will have the units of length cubed [L 3 ]. )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 (Last, we will check all of our dimensions by using the allowable deformation. )Tj ET 0 G 0 J 0 j 0.501 w 10 M []0 d 1 i 304.63 219.831 m 320.893 219.831 l S BT /F9 1 Tf 12.009 0 2.642 12.034 270.136 216.729 Tm (d)Tj 12.009 0 0 12.034 280.425 216.729 Tm (=)Tj 18.014 0 0 18.051 290.119 214.002 Tm (\345)Tj /F7 1 Tf 12.009 0 0 12.034 306.006 224.281 Tm (PL)Tj -0.0156 -1.3906 TD (EA)Tj /F4 1 Tf 12 0 0 12 322.081 216.737 Tm ( $4$)Tj -19.34 -2.98 TD 0.0002 Tw (In this case the design is more open-ended. 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. )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. ` @!! E @ I! d= ] I! d= ] I! d= ]!... ( concentrations strength, stiffness, and also the formula for axial load, stress!, 76 ( 2018 ) % 'Tj\YQQ6V $ tLSn @: ZkQ # Z4^ will! The eccentrically loaded column specimens, the lateral displacement due to axial,. 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