i need support for my study task: a tiny rocket dia 4mm, length 60mm, needs a laminar flow that "sucks" the airflow into the center axis behind the projectile´s tail.
the task is 1. to show the "coanda" effect at different velocities (0-M3), and 2. how this effect can be locally disturbed by what forces applied, and 3. how the thrust jet is influenced/squeezed by the orthogonal pressure vector caused by the coanda effect.
please only apply if you are a fluid dynamics specialist.
17 freelanceria on tarjonnut keskimäärin 176$ tähän työhön
hi. i have read all your description. im a expert in cfd simulation( ansys cfx) im a master in turbomachinery i can do it well for you. i hope we will work together. thank you for your posting.