Abstract
The basic position described above concerning methods of calculating aerodynamic characteristics of isolated wings remains in force in the consideration of the motion of a wing close to an interface.
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© 1967 Springer Science+Business Media New York
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Belotserkovskii, S.M. (1967). Controls Attached to Monoplane Wings. The Effect of Interface. In: The Theory of Thin Wings in Subsonic Flow. Springer, Boston, MA. https://doi.org/10.1007/978-1-4899-6299-7_13
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DOI: https://doi.org/10.1007/978-1-4899-6299-7_13
Publisher Name: Springer, Boston, MA
Print ISBN: 978-1-4899-6161-7
Online ISBN: 978-1-4899-6299-7
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