I am looking for someone to write a script to automate running CFD on multiple NACA Airfoils to determine the drag coefficient of each airfoil.
The NACA airfoil data will be delivered in a Selig format dat file such as:
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The script will take as an input the path to a folder containing multiple NACA airfoil .dat files. The script will automatically set up the CFD case, run the CFD case and output the coefficient of drag for the airfoil to a text file.
The CFD case is to be run on air at 70 degC, sea level at a Reynolds Number of 3,000,000
The CFD tool to be used in this implementation is to be agreed upon by the freelancer and myself.
The script coordinating the automation will preferably be written in python.
11 freelancers are bidding on average $184 for this job
Hello I'm a masters degree holder in aerospace engineering. I'm experienced in CFD and i constructed this code before. Lemme know more about ur project, expected budget and deadline.
Hi, I'm interested in taking up your project. I have done 10+ projects in software development and scripts and utilities using python. I delive fast,clean [login to view URL] forward to your response
Hi sir, I have experience on CFD project. I will do your project as per requirement. I am using the Ansys Workbench and Starccm+ for CFD analysis. I will do the final report as per your requiment.