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Free-to-Roll Oscillations of Low Aspect Ratio Wings


Reference:

Gresham, N. T., 2010. Free-to-Roll Oscillations of Low Aspect Ratio Wings. Thesis (Doctor of Philosophy (PhD)). University of Bath.

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    Details

    Item Type Thesis (Doctor of Philosophy (PhD))
    CreatorsGresham, N. T.
    Uncontrolled Keywordsoscillations, aerodynamics, delta, non-slender
    DepartmentsFaculty of Engineering & Design > Mechanical Engineering
    Publisher StatementUnivBath_PhD_2010_N_Gresham.pdf: © The Author; UnivBath_PhD_2010_N_Gresham_AppB.pdf: © The Author
    StatusUnpublished
    ID Code27095

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