Determination of Parameters during Quasi-Steady Stall Maneuver Using Genetic Algorithm
<p>The current work offers the determination of longitudinal aerodynamic derivatives during flight manoeuver at angles of attack near the stall. The flight manoeuver near stall is highly non-linear in nature due to separated flow at such elevated angles of attack. Kirchoff’s model for Quasi-Steady S...
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| Asıl Yazarlar: | , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
Embry-Riddle Aeronautical University
2019-01-01
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| Seri Bilgileri: | International Journal of Aviation, Aeronautics, and Aerospace |
| Konular: | |
| Online Erişim: | https://commons.erau.edu/ijaaa/vol6/iss4/4 |
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