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Numerical Investigation of Flow Control over an Airfoil: Synthetic Jet and Its Optimization Eray Akçayöz
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Numerical Investigation of Flow Control over an Airfoil: Synthetic Jet and Its Optimization
Eray Akçayöz
The synthetic jet is applied over an airfoil to control the flow separation. Response Surface Methodology is employed for the optimization of synthetic jet parameters at various angles of attack. The synthetic jet parameters; the jet velocity, the jet location, the jet angle and the jet frequency are optimized to maximize the lift to drag ratio. The jet power coefficient is kept constant in the optimization. The lift to drag ratio increased significantly especially at post stall angles of attack.
| Mediji | Grāmatas Paperback Book (Grāmata ar mīksto vāku un līmēto muguru) |
| Izlaists | 2010. gada 6. jūlijs |
| ISBN13 | 9783838356013 |
| Izdevēji | LAP Lambert Academic Publishing |
| Lapas | 88 |
| Izmēri | 225 × 5 × 150 mm · 149 g |
| Valoda | Vācu |
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