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• W2314202376 abstract "The goal of the current study was to determine if computational fluid dynamics is capable of accurately predicting the forces and moments on the F/A-18E Super Hornet at the high-lift aerodynamic conditions usually encountered during carrier landing. Past F/A18E computational studies have mainly focused on wind-tunnel scale calculations with the results being compared to existing wind-tunnel data. The calculations for this study were conducted at full scale and the results were compared to F/A-18E sim data where possible. The computational geometry included all of the flaps, control surfaces, shrouds and gaps usually present on the actual aircraft. During this study, static calculations were completed at various F/A-18E conditions along the path of an untrimmed longitudinal stick doublet maneuver. These calculations represent small, medium and large trailing-edge flap deflections. The results were compared to F/A-18E sim data. In addition, several static calculations were conducted for the F/A-18E trimmed with two different sets of control laws at three different longitudinal stick positions. Once again, these results were compared to F/A-18E sim data. Finally, a study was conducted to determine the effect of the trailing-edge flap deflection, aileron deflection and angle of attack on the F/A-18E forces and moments. A wide range of trailing-edge flap deflections was considered. Overall, the comparisons between the computational results and the sim data were favorable. However, the correlations for the pitching moment indicate that there is room for improvement. Traditionally, accurately predicting the pitching moment on the F/A-18E has been very challenging." @default.
• W2314202376 created "2016-06-24" @default.
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• W2314202376 date "2016-01-02" @default.
• W2314202376 modified "2023-09-26" @default.
• W2314202376 title "CFD Analysis of the F/A-18E Super Hornet during Aircraft-Carrier Landing High-Lift Aerodynamic Conditions" @default.
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• W2314202376 doi "https://doi.org/10.2514/6.2016-1768" @default.
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