Week 13 and week 14: Fabricating the Prototype and Work on the Finite Element Analysis
In these two weeks, I focused on building the prototype and finishing up the FEA for the solar rack. For building the prototype, I meet up with my team to fabricate the prototype and to figure out the best way to building the parts faster. Below is the progress that I make so far on the hand-calculation drag coefficient and drag lift. These data will be implemented in ANSYS to run for the FEA in next couple days. Source: https://file.scirp.org/pdf/JFCMV_2016012909451497.pdf Wind analysis including cooling effects and lift prevention. D d = C d ⍴ V 2 2 A D l = C l ⍴ V 2 2 A Where D d is wind drag D d , D l : drag and lift forces, C d , C l : drag and lift coefficient relatively, ⍴ is the density of air, V is velocity of wind which has V peak and V storm , and A is the reference area or cross-sectional area of the lowest point of calcul. Wind load calculation has to be calculated using the following values. ⍴ = 1.225 kg/m 3 , V could be replaced by V peak