Write a technical report for CFD homework by analysing and modifying the aerodynamic performance of a NACA 4412 airfoil. The assignment details are listed in the attached file named “Details”. Also, an example is attached to understand the reequipment not to follow it where it is for different NACA and speed.
In addition, the marking criteria for the report is attached to follow while and after doing the report.
Important note: The maximum pages is 13 for the main report including figures and tables that excluding cover page, table of contents and references.
You are required to submit the technical report along with “AI” and “turnitin” report for similarity where you shall have low similarity percentage and 0 ZERO percentage for plagiarism. Also, the software used for the CFD model shall be submitted (All files).
Please read the instructions carefully, and let me know if you have any question.
Requirements: The maximum pages is 13 for the main report including figures and tables that excluding cover page, table of contents and references
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