Introduction to Aerodynamics

Catalog description

Pressure distribution and forces on aerodynamic shapes are predicted by using potential flow theory. Incompressible, potential flow governing equations are derived. Equations representing uniform flow, vortices, and potential flow sources are developed, and used to study velocity and pressure fields in some common external flows including airfoils. The study of boundary layers and how they affect the performance of lifting surfaces will be covered. Additionally, a panel method computer code is developed to predict pressure distribution and lift and drag forces on an arbitrary airfoil. Cross-listed with MECG 608 .