Abstract
In investigations of three-dimensional airfoils (monoplane and annular wings), we use a standard coordinate system fixed in the wing (Fig. 1.1). This consists of a rectangular right-handed Cartesian system with the Ox axis directed along the wing axis and the Oy axis in the plane of symmetry of the wing.
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© 1967 Springer Science+Business Media New York
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Belotserkovskii, S.M. (1967). General Considerations. In: The Theory of Thin Wings in Subsonic Flow. Springer, Boston, MA. https://doi.org/10.1007/978-1-4899-6299-7_1
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DOI: https://doi.org/10.1007/978-1-4899-6299-7_1
Publisher Name: Springer, Boston, MA
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