Presentation BL
11
Laminar Boundary- Layer with an arbitrary pressure gradient Ademar Nunes Gilberto Luque Renan Santos
Transcript of Presentation BL
S
Laminar Boundary-Layer with an arbitrary
pressure gradient Ademar Nunes Gilberto Luque Renan Santos
Main Goal
S Analyze Drag of NACA 4 digits airfoils.
Methodology
Methodology
Methodology
Results
Results (NACA 0009)
Results (NACA 0012)
Results (NACA 2412)
Results (NACA 4412)
Questions?
