a tiny rocket dia 8mm, length 60mm, needs a laminar flow that "sucks" the airflow into the center axis behind the projectile´s tail which therefore gets a coanda form.
the task is 1. to show the "coanda" effect at different velocities (0-<mach0.5), 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, and 4. How a turn rate would be, forces, etc.
please only apply if you are a fluid dynamics specialist.
Task1 should be done in august, last task finished in September/october.
look a the xls sheet for more info
20 фрилансеров(-а) готовы выполнить эту работу в среднем за $1128
I am mathematician specialist in fluid dynamic with three years of experience at industry at teaching at the university as professor. I am use to work with Matlab or octave to make the experiments and obtain results.
Hi, there. I am a CFD engineer with 5+ years of hands-on experience. Carefully checked your requirements, I think I am capable of doing this job. Hope to have a chance to discuss. Best regards, Sgadou
Hello, I am CFD expert. I checked your file. I have an experience in the numerical simulation with ANSYS Fluent, CFX and also I have done project like this. I am sure I can complete your project ON TIME. Thanks.