Composite beam is overhanging beam which is aircraft spar. Loads need to calculate as the pressure applicable on the spar
37 freelanceria on tarjonnut keskimäärin %project_bid_stats_avg_sub_26% %project_currencyDetails_sign_sub_27% tähän työhön
Dear. I am a professional in Structural mechanics and FEA. I am sure I can do it. I can use ANSYS/ABAQUS/MATLAB/C/C++/... We can discuss about details via chat. I wait for your response. Thanks.