I need help with a mini project of aerospace engineering : aircraft performance : aircraft stability and control : technical report writing : aerospace propulsion and turbo machinery : vibration : Finite element method ( matlab coding) Need experience in these subjects
To find the best fit of the line to compute the endpoint. The knowns are points coordinates aligned together and aligned with the wanted endpoint. The 3D coordinates of the endpoint (XYZ) are wanted to calculated and adjusted.
You have been assigned with the design of a composite shell for the wing of PC9 aircraft. Under Design Limit Load (DLL), the composite laminate is subjected to given ??, ?? and ???. The laminate configuration based on the aerospace design guidelines is required. Assume that zero and 90-degree plies do not contribute towards the shear strength of the laminate. Part A: Determining failure properties...
It′s a design project of a satellite system for a space system engineering class. So, you need to have some engineering experience or knowledge. Also, you need to be good at math. Another thing, I′m not sure if you need to add some outsources other than the sources that are listed on the project desсrіption. I need it in 48 hrs max.