UZB 362E - Sıkıştırılabilir Aerodinamik

Dersin Amaçları

• To define compressibility and its effects on fundamental flow equations
• To teach students shock and expansion waves and related calculation methods
• To teach students linearization of fundamental equations and the conditions under which they apply
• To furnish the students with the ability to calculate the flowfield and aerodynamic forces in compressible flow

Dersin Tanımı

Two dimensional subsonic compressible steady and isentropic flows. Normal shocks. Oblique shocks. Expansion waves. Compressible flow through nozzles, diffusers, and wind tunnels. Linear theory for subsonic and supersonic flows. Supersonic airfoils. Elements of hypersonic flow.