| Kodu | Dersin Adı | Yarıyıl | Süresi(T+U) | Kredisi | AKTS Kredisi |
|---|---|---|---|---|---|
| UCK302 | AERODİNAMİK II | 6 | 4 | 3 | 4 |
AMAÇ VE İÇERİK |
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|---|---|
| Amaç: | To teach the effects of compressibility on aerodynamic phenomena in high-speed subsonic flows and their calculations, the calculation methods for vertical shock, oblique shock and expansion waves in supersonic flows, and the numerical methods for calculations in supersonic flows. |
| İçerik: | Thermodynamic reminders. Equations for compressible one-dimensional flows, normal shock waves. Oblique shock and expansion waves. Squat one-dimensional flows. Flows in pipes and wind tunnels. Linearized theory for compressible potential flows. Correction formulas for subsonic compressible flows. Linearized theory for supersonic flows. Characteristics method for supersonic flows. |