please help me with matlab!!
Q1. Tensile Mechanics- Analysis of Data (refer to Contents / Week 4 / Assignments/Assessments/Case- Study_Rotator-Cuff_Tensile-Mechanics-Data.xls): You have designed a new matrix for augmentation of rotator cuff repairs. To verify that your design meets the mechanical requirements, you perform uniaxial tensile testing. Before scaling up your design, you choose to conserve resources and construct a small sample of your material that measures just 1.581 mm2 in cross-sectional area (CSA) with a gauge (original, undeformed) length of 8 mm. The force and displacement data recorded by the mechanical testing machine are provided in a separate spreadsheet. Compute 1) ultimate tensile strength, 2) ultimate strain, and 3) elastic modulus from the linear region. Q2. Considering mechanical parameters such as ultimate tensile strength, ultimate strain, and linear region modulus of elasticity, does your new matrix meet the requirements? To make a justified conclusion, compare your results to available literature on rotator cuff tendon mechanical properties or benchmarking of other commercially available rotator cuff repair patches. Aurier DP B Case Study Rotator-C.ET_Tensit-Mechanics Data Protected VIEN Search A cuy | Fle Home Insert Page Layout Formulas Data Revic View Hep Share Comments PROTECTED VIEW Becardul files from the Internet can contain viruses. Unless you need to cecit. it's safe to stay in Protected View Erable Edling K14 be c D E F H 1 J N N P R S U w V w X Y 7 AA AB 1 1 Matrix Tensile Testing 2 Gauge length 3mm 3 CSA 1.501 mm Timesec) Disp [mm] Load (N) 6. 0 0 0.09994378 7 0 0.09324378 8 0.118 0 0.09370339 9 0.37 0.0020671 0.07012917 10 0.432 0.0089968 0.10086293 11 1.090 0.02009506 0.09544614 12 1.5R6 OLOGR00226 0.1255605 13 2.035 0.04899474 0.12380071 14 2.010 0.00300933 0.16112852 15 3.167 0.07510207 0.17003 M3 0.170M 16 3.674 0.08799679 0.19373866 17 4.394 0.10602919 0.25830059 18 4.906 0.11694 0.24101657 AM 19 5.446 0.13108799 0.32833661 5,958 0.14259UZ 0.37134389 21 6.60 0.157941-44 0.4482111 22 7.102 017000064 0.52081724 7.002 0.19059210 0.58915400 94 8.107 0.19394518 0.66204234 8.GOZ 0.20398990 0.73206202 9.102 0.21900109 0.77921100 77 4.63 023094916 0.0126637 28 10.132 0.24302484 0.90381294 10.032 0.25390252 1.00504007 30 11.5 0.27596935 1.25188915 31 12 0.28719546 1.40192966 12.018 0.30310319 1.550379 re 33 13.16 0.120001 1.857316M 34 14.02 0.33607078 2.09927303 14.52 0.34750962 2.34307150 36 1.5.0.2 0.359A4 2.51097 37 15.758 0.37799466 2.91517726 38 10.002 0.39777311 3.3452004 19 17.100 0.40994503 1.64774190 18.054 0.4329929 4.26419778 41 19.594 0.44379 0.44 4.56527201 Matrix Tensile Testing 115 WARS 40 + 100% Type here to search O 1:24 PM 2/10/2021 0 Aurinn DU Case Study Rotator-C.ET_Tensit-Mechanics Data Protected VIEN Search A cuy Fle Home Insert Page Layout Formulas Data Revic View Hep Share Comments PROTECTED VIEW Becardul files from the Internet can contain viruses. Unless you need to cecit. it's safe to stay in Protected View Erable Edling K14 G 4 D E F H 1 M N R S U V w Y 7 AA AB 10 41 13 44 45 16 47 48 19 50 51 52 54 55 57 00 61 18.051 0.1329929 1.26119778 18.554 0.44399348 4.56527201 19.054 0.45700046 4.99197561 19.551 016704813 5.31221251 20.268 0.48608343 5.93209406 21.250 0.5099957 0.77343225 21.756 O52196222 7.26861079 22.256 0.53099691 7.5828773 22.834 0.34707374 8.21204823 23.722 0.5685299 9.15551001 24.222 0.57998907 9.59732197 24.76 0.59397207 10.24834019 25.26 0.6108701 10.749001123 25.76 0.61799139 11.32792793 20.71 0.03999401 12.35615452 27.21 0.65226695 12.968756 27.71 O.GG300007 13.55648413 29.494 0.08320837 14.45541717 29.186 0.69%8714 15.19756019 29.696 0.71198779 15.78100957 30.156 0.72399059 10.308754 31.1.46 0.7605287 17.3318293 31.646 0.73899134 17.84743970 32.146 0.72099946 19.3946453 32.646 0.73194092 18.77966151 33.146 0.79499031 19.36318539 33.718 0.80908539 19.91984907 31.218 0.81%29972 20.3160741 34.718 0.83298972 20.88133240 35.218 0.84399109 21.10943073 35.718 0.8567851 21.71512531 36.218 0.86799568 22.0965147 30.940 0.88599810 22.70786545 37.596 090168107 23.1929312 38.096 0.91395784 23.557655SI 39.042 0.93090309 24.15901213 39.77 0.95180M 2.35250MA 40.282 OSG709737 24.82303166 40.752 0.97902999 23.00789645 11.2R2 098877063 25.13971905 41.784 1.00298645 25.47243051 mu 64 00 28 70 71 73 74 73 76 77 78 79 30 Matrix Tensile Testing + 100% Type here to search O 1:24 PM 2/10/2001 D Auri 0 B Case Study Rotator-C.ET_Tensit-Mechanics Data Protected VIEN Search A cuy Fle Home Insert Page Layout Formulas Data Revic View Hep Share Comments PROTECTED VIEW Becardul files from the Internet can contain viruses. Unless you need to cecit. it's safe to stay in Protected View Erable Edling K14 be D E F H 1 M N R S U V w Y 7 AA AB 81 84 26 87 41.271.002105 25.1222051 41.92 1.00596437 25.5G16G798 42.42 1.01758752 25.5008019 13.351 1.091000001 25.16521851 43.854 1.05198862 25.0341BSS 44.354 1.00412907 25.07173500 11.892 1.0779833 2.83186312 45.402 1.08930775 24.2751576 45.914 1.1039876 22.99270593 17.051 1.129.88R2 16.77511632 47.554 1.13906776 15.72744548 49.064 1.15323027 15.8302008 18.0 1.15YAM7 15.0251265 48.584 1.16598719 15.5174145 49.054 1.17098645 15.53443811 19.556 1.1841166 15.7776 49.64 1.19108775 15.75634442 49.654 1.19099253 15.70210372 19 20 91 92 94 97 90 20 100 101 102 103 104 105 100 107 108 109 110 112 113 115 116 117 110 119 120 Matrix Tensile Testing + 100% Type here to search O 125 PM 2/10/2001 D Q1. Tensile Mechanics- Analysis of Data (refer to Contents / Week 4 / Assignments/Assessments/Case- Study_Rotator-Cuff_Tensile-Mechanics-Data.xls): You have designed a new matrix for augmentation of rotator cuff repairs. To verify that your design meets the mechanical requirements, you perform uniaxial tensile testing. Before scaling up your design, you choose to conserve resources and construct a small sample of your material that measures just 1.581 mm2 in cross-sectional area (CSA) with a gauge (original, undeformed) length of 8 mm. The force and displacement data recorded by the mechanical testing machine are provided in a separate spreadsheet. Compute 1) ultimate tensile strength, 2) ultimate strain, and 3) elastic modulus from the linear region. Q2. Considering mechanical parameters such as ultimate tensile strength, ultimate strain, and linear region modulus of elasticity, does your new matrix meet the requirements? To make a justified conclusion, compare your results to available literature on rotator cuff tendon mechanical properties or benchmarking of other commercially available rotator cuff repair patches. Aurier DP B Case Study Rotator-C.ET_Tensit-Mechanics Data Protected VIEN Search A cuy | Fle Home Insert Page Layout Formulas Data Revic View Hep Share Comments PROTECTED VIEW Becardul files from the Internet can contain viruses. Unless you need to cecit. it's safe to stay in Protected View Erable Edling K14 be c D E F H 1 J N N P R S U w V w X Y 7 AA AB 1 1 Matrix Tensile Testing 2 Gauge length 3mm 3 CSA 1.501 mm Timesec) Disp [mm] Load (N) 6. 0 0 0.09994378 7 0 0.09324378 8 0.118 0 0.09370339 9 0.37 0.0020671 0.07012917 10 0.432 0.0089968 0.10086293 11 1.090 0.02009506 0.09544614 12 1.5R6 OLOGR00226 0.1255605 13 2.035 0.04899474 0.12380071 14 2.010 0.00300933 0.16112852 15 3.167 0.07510207 0.17003 M3 0.170M 16 3.674 0.08799679 0.19373866 17 4.394 0.10602919 0.25830059 18 4.906 0.11694 0.24101657 AM 19 5.446 0.13108799 0.32833661 5,958 0.14259UZ 0.37134389 21 6.60 0.157941-44 0.4482111 22 7.102 017000064 0.52081724 7.002 0.19059210 0.58915400 94 8.107 0.19394518 0.66204234 8.GOZ 0.20398990 0.73206202 9.102 0.21900109 0.77921100 77 4.63 023094916 0.0126637 28 10.132 0.24302484 0.90381294 10.032 0.25390252 1.00504007 30 11.5 0.27596935 1.25188915 31 12 0.28719546 1.40192966 12.018 0.30310319 1.550379 re 33 13.16 0.120001 1.857316M 34 14.02 0.33607078 2.09927303 14.52 0.34750962 2.34307150 36 1.5.0.2 0.359A4 2.51097 37 15.758 0.37799466 2.91517726 38 10.002 0.39777311 3.3452004 19 17.100 0.40994503 1.64774190 18.054 0.4329929 4.26419778 41 19.594 0.44379 0.44 4.56527201 Matrix Tensile Testing 115 WARS 40 + 100% Type here to search O 1:24 PM 2/10/2021 0 Aurinn DU Case Study Rotator-C.ET_Tensit-Mechanics Data Protected VIEN Search A cuy Fle Home Insert Page Layout Formulas Data Revic View Hep Share Comments PROTECTED VIEW Becardul files from the Internet can contain viruses. Unless you need to cecit. it's safe to stay in Protected View Erable Edling K14 G 4 D E F H 1 M N R S U V w Y 7 AA AB 10 41 13 44 45 16 47 48 19 50 51 52 54 55 57 00 61 18.051 0.1329929 1.26119778 18.554 0.44399348 4.56527201 19.054 0.45700046 4.99197561 19.551 016704813 5.31221251 20.268 0.48608343 5.93209406 21.250 0.5099957 0.77343225 21.756 O52196222 7.26861079 22.256 0.53099691 7.5828773 22.834 0.34707374 8.21204823 23.722 0.5685299 9.15551001 24.222 0.57998907 9.59732197 24.76 0.59397207 10.24834019 25.26 0.6108701 10.749001123 25.76 0.61799139 11.32792793 20.71 0.03999401 12.35615452 27.21 0.65226695 12.968756 27.71 O.GG300007 13.55648413 29.494 0.08320837 14.45541717 29.186 0.69%8714 15.19756019 29.696 0.71198779 15.78100957 30.156 0.72399059 10.308754 31.1.46 0.7605287 17.3318293 31.646 0.73899134 17.84743970 32.146 0.72099946 19.3946453 32.646 0.73194092 18.77966151 33.146 0.79499031 19.36318539 33.718 0.80908539 19.91984907 31.218 0.81%29972 20.3160741 34.718 0.83298972 20.88133240 35.218 0.84399109 21.10943073 35.718 0.8567851 21.71512531 36.218 0.86799568 22.0965147 30.940 0.88599810 22.70786545 37.596 090168107 23.1929312 38.096 0.91395784 23.557655SI 39.042 0.93090309 24.15901213 39.77 0.95180M 2.35250MA 40.282 OSG709737 24.82303166 40.752 0.97902999 23.00789645 11.2R2 098877063 25.13971905 41.784 1.00298645 25.47243051 mu 64 00 28 70 71 73 74 73 76 77 78 79 30 Matrix Tensile Testing + 100% Type here to search O 1:24 PM 2/10/2001 D Auri 0 B Case Study Rotator-C.ET_Tensit-Mechanics Data Protected VIEN Search A cuy Fle Home Insert Page Layout Formulas Data Revic View Hep Share Comments PROTECTED VIEW Becardul files from the Internet can contain viruses. Unless you need to cecit. it's safe to stay in Protected View Erable Edling K14 be D E F H 1 M N R S U V w Y 7 AA AB 81 84 26 87 41.271.002105 25.1222051 41.92 1.00596437 25.5G16G798 42.42 1.01758752 25.5008019 13.351 1.091000001 25.16521851 43.854 1.05198862 25.0341BSS 44.354 1.00412907 25.07173500 11.892 1.0779833 2.83186312 45.402 1.08930775 24.2751576 45.914 1.1039876 22.99270593 17.051 1.129.88R2 16.77511632 47.554 1.13906776 15.72744548 49.064 1.15323027 15.8302008 18.0 1.15YAM7 15.0251265 48.584 1.16598719 15.5174145 49.054 1.17098645 15.53443811 19.556 1.1841166 15.7776 49.64 1.19108775 15.75634442 49.654 1.19099253 15.70210372 19 20 91 92 94 97 90 20 100 101 102 103 104 105 100 107 108 109 110 112 113 115 116 117 110 119 120 Matrix Tensile Testing + 100% Type here to search O 125 PM 2/10/2001 D
