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- W2016115063 abstract "An extensions of empirical model of vortex breakdown position on delta wing under sideslip condition is presented. Extension of vortex breakdown to sideslip condition can be useful for empirical aerodynamic coefficients determination. Comparison to experimental data shows that the model provides good approximation. > Γ α Circulation at trailing edge at angles of attack beyond that at which breakdown occurs at the TE" @default.
- W2016115063 created "2016-06-24" @default.
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- W2016115063 date "2003-06-22" @default.
- W2016115063 modified "2023-09-26" @default.
- W2016115063 title "An Empirical Model for Delta Wing Vortex Breakdown Location in Sideslip Condition" @default.
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- W2016115063 doi "https://doi.org/10.2514/6.2003-5398" @default.
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