Flow around aerodynamic body

Ovaj rad bavi se aerodinamikom aviona. Prvi dio rada odnosi se na izradu 3D modela aviona s prilagođenim novim krilom, odnosno NACA 2411 profilom u programu Autodesk Inventor. Nakon izrade 3D modela, korišten je Hypermesh za izradu numeričke mreže. Dobivena numerička mreža ubačena je u Virtual Wind Tunnel gdje je provedeno nekoliko simulacija koje su uspoređene i na temelju kojih su doneseni zaključci.The topic of this final thesis is the aerodynamics of airplanes. The first part refers to the creation of a 3D model of the airplane with an adapted new wing NACA 2411 profile in the Autodesk Inventor program. After a 3D model was created, Hypermesh was used to create the numerical mesh. The resulting numerical network was inserted into Virtual Wind Tunnel, where several simulations were performed, compared, and based on which conclusions were drawn