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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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Hlavní autoři: AMBUJ SRIVASTAVA, Ajit Kumar, Ajoy Kanti Ghosh
Médium: Artigo
Jazyk:Inglês
Vydáno: Embry-Riddle Aeronautical University 2019-01-01
Edice:International Journal of Aviation, Aeronautics, and Aerospace
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On-line přístup:https://commons.erau.edu/ijaaa/vol6/iss4/4
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