I need help solving this question, I'm stumped on where to even begin:
Describe the equilibrium condition that occurs at the grips of the figure shown:
\f2 Material Aluminum Sample Information: L 53.89 mm Length, length of sample between grips W 12.59 mm Width 3.33 mm Thickness LO 53.89 mm Gage Length, the length used for elongation measurements Displacement and Force Data: 10 dL from Crosshead to rupture; P is axial force. 11 12 dL P 13 mm N 14 0.011018 2924.593 15 0.019416 3083.676 16 0.027873 3244.429 17 0.036212 3402.977 18 0.044609 3554.248 19 0.053007 3705.143 20 0.061464 3854.638 21 0.069922 4002.243 22 0.07832 4150.036 23 0.086777 4291.987 24 0.095115 4435.465 25 0.103572 4576.987 26 0.11203 4715.935 27 0.120427 4854.868 28 0.128825 4990.093 29 0.137283 5124.205 30 0.14568 5256.042 31 0.154138 5386.156 32 0.162535 5517.667 33 0.170993 5648.564 34 0.17945 5778.943 35 0.187848 5904.998 36 0.196365 5990.703 37 0.204762 6113.098 38 0.21316 6241.034 39 0.221618 6365.595 40 0.230015 6490.02441 0.238473 6612.941 42 0.24687 6733.96 43 0.255328 6858.592 44 0.263845 6977.62 45 0.272302 7101.087 46 0.2807 7216.677 47 0.289157 7333.753 48 0.297555 7450.051 49 0.306012 7561.756 50 0.314469 7680.014 51 0.322867 7793.247 52 0.331324 7904.84 53 0.339722 8017.061 54 0.34818 8130.403 55 0.356577 8241.301 56 0.365035 8353.072 57 0.373492 8462.254 58 0.38189 8573.378 59 0.390347 8683.505 60 0.398804 8792.615 61 0.407202 8898.306 62 0.415719 9002.937 63 0.424117 9112.497 64 0.432574 9217.512 65 0.440972 9321.765 66 0.449429 9427.785 67 0.457887 9529.948 68 0.466403 9636.486 69 0.474801 9739.529 70 0.483258 9840.214 71 0.491656 9938.768 72 0.500114 10036.5 73 0.508571 10127.44 74 0.517028 10225.09 75 0.525426 10317.14 76 0.533824 10408.95 77 0.542281 10500.64 78 0.550738 10591.32 79 0.559255 10683.3 80 0.567653 10772.8981 0.57611 10861.06 82 0.584449 10949.53 83 0.592906 11037.19 84 0.601363 11 123.85 85 0.609821 11208.97 86 0.618278 11293.07 87 0.626676 11376.69 88 0.635073 11459.88 89 0.64359 11542.24 90 0.652048 11624.08 91 0.660505 11704.44 92 0.668903 11783.16 93 0.67736 11859.02 94 0.685817 11933.28 95 0.694275 12006.85 96 0.702732 12074.08 97 0.711189 12141.67 98 0.719587 12204.51 99 0.728044 12261.2 100 0.736442 12313.55 101 0.744959 12359.25 102 0.753416 12399.36 103 0.761933 12434.06 104 0.770331 12464.28 105 0.778729 12490.68 1061 0.787186 12515.04 107 0.795643 12536.71 108 0.80416 12556.13 109 0.812618 12573.18 110 0.821075 12588.74 111 0.829473 12601.8 112 0.83799 12616.37 113 0.846447 12626.75 114 0.854964 12637.94 115 0.863421 12646.49 116 0.871878 12656.34 117 0.880336 12664.03 118 0.888793 12672.51 119 0.89725 12679.41 120 0.905767 12686.26121 0.914224 12692.68 122 0.922682 12698.27 123 0.931139 12704 97 124 0.939656 12710.37 125 0.948173 12714.11 126 0.956571 12719.54 127 0.965088 12723.96 128 0.973426 12726.3 129 0.981883 12732.13 130 0.9904 12736.11 131 0.998857 12740.01
