Im looking for someone to do ANSYS simulation of airfoil NACA 0015. (2d simulation)
1. i need values of Lift and drag coefficient in laminar flow for Angle of attack (0,1,2,3,4,5...20 degree)
2. i need values of lift and drag coefficient in k-e flow for the same AoA (0-20 degree)
cord lenght of foil is 100mm, also domaine need to be c shape (picture in attachment)
and be careful with y+ values.
Also it imporant that angle of airflow is changing, and not rotation of airfoil
i need need all files and,datas, and graphs
ansys file in attachment,
mesh is done correctly, but mistake is made in setup or maybe in drawing of foil.
you can check it
also wind speeds for every angle needs to be : 2,4,6,8,10,12,14,16,18,20 m/s
22 freelancers are bidding on average €90 for this job
Hi, I am Aerospace Engineer with extensive experience in cfd analysis of aircraft wings, airfoil shaped blades, rotors etc. Kindly visit portfolio and provide more details in chat.
hi. im a master in turbomachinery. i have done thousands simulation like this. you can check my profile to see some my simulation. i can do it well for you. thank you for your posting!
I just recently completed a similar project so I am certain that I can assist you with this project. I'm a Mechanical engineer with a precise knowledge of ANSYS software.