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- W2077455784 abstract "spin rate or asymmetric shedding of the body vortices. Both nonlinearities due to spin rate and asymmetric vortices appear to be significant at Mach numbers below 1.5 and angles of attack greater than about 20 deg. Comparison of the new method with existing experimental databases was very encouraging. However, additional data on various configurations (particularly wing–body–tail cases) are needed for further validation and refinement of the semiempirical model. Nomenclature Aref = reference area (maximum cross-sectional area of the body, with the body present, or of the planform area of the wing, with the wing alone), ft 2 AW = wing planform area, ft 2 = aspect ratio b = wing span (not including body), ft C‘ = roll moment coefficient C‘P = roll damping moment coefficient" @default.
- W2077455784 created "2016-06-24" @default.
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- W2077455784 date "2008-09-01" @default.
- W2077455784 modified "2023-09-27" @default.
- W2077455784 title "New Method to Predict Nonlinear Roll Damping Moments" @default.
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- W2077455784 doi "https://doi.org/10.2514/1.34974" @default.
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