Akademik Dersler - İçerik

Apply the basic principles of aerodynamics.
Use Bernoulli's principle, conservation of mass and Newton's laws in the context of fluid flow.
Analyze different flow regimes encountered in aerodynamics.
Calculate the aerodynamic forces on a body considering both steady and variable flow conditions.
Explain the principles of profile theory.
Describe the mechanisms of lift force generation.
Explain stall conditions and the concept of circulation around the profile.
Analyze the methods and techniques to reduce drag force.
List the methods of boundary layer control.
Explains advanced drag reduction methods.
5. Evaluate the performance of wings and wing configurations for different applications, taking into account factors such as aspect ratio, sweep angle and wing tip design.
Analyze aerodynamic behavior using computational methods such as computational fluid dynamics (CFD).
Explain the principles of stability and control of aircraft and spacecraft.
Analyze aerodynamic phenomena at high speeds.
Describe supersonic and hypersonic flow regimes.
Explain shock waves and aerodynamic heating effects.