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- W3110147663 abstract "A study has been made of the unusual results obtained in large-amplitude oscillatory coning and pitching tests of a generic combat aircraft model. The analysis shows that the observed highly nonlinear effects of angular amplitude and rate on the unsteady aerodynamics can be explained by using the knowledge of unsteady separated e ow physics gained from one-degree-of-freedom dynamic experiments. Anomalous effects are produced by the wind-tunnel testing practice of using boundary-layer trips, which introduces a unique sensitivity to boundarylayer transition not found in full-scale e ight." @default.
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- W3110147663 date "1998-01-12" @default.
- W3110147663 modified "2023-09-27" @default.
- W3110147663 title "Nonlinear rate and amplitude effects on a generic combat aircraft model" @default.
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- W3110147663 doi "https://doi.org/10.2514/6.1998-409" @default.
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