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- W1983679689 abstract "An experimental contribution to the investigation of the wing rock phenomenon is presented. Free to roll experiments and flow visualizations were performed on a 80° delta wing, at different subsonic airspeeds and angles of attack. The relevant aspects of the limit cycle characteristics are analyzed on the basis of the experimental evidence. Some comparisons among the results of similar experiences carried out in different laboratories are introduced and discussed. An analytical nonlinear formulation of the differential equation governing the single degree of freedom approximation of the roll mode was validated." @default.
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- W1983679689 date "1997-02-01" @default.
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- W1983679689 title "Experimental observation and discussion of the wing rock phenomenon" @default.
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- W1983679689 doi "https://doi.org/10.1016/s1270-9638(97)90041-9" @default.
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