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- W2992443818 abstract "A theoretical investigation of the rolling motion of triform configurations at high angles of attack is presented. A nonlinear aerodynamic flow model, derived from strip and slender body theories, ..." @default.
- W2992443818 created "2019-12-13" @default.
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- W2992443818 date "2016-06-10" @default.
- W2992443818 modified "2023-10-16" @default.
- W2992443818 title "Nonlinear Rolling Motion of Triform Finned Missiles" @default.
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- W2992443818 doi "https://doi.org/10.2514/6.2016-4334" @default.
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