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Equations for Determination of the Strength of a Bound Vortex Sheet

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Abstract

By using the formulas given in the preceding chapter for an infinite vortex chain, we can obtain expressions for the disturbed velocities in the fluid about a cascade of thin profiles. We replace each profile by a continuous distribution of vortex sheets of strength Γ (s). We use the coordinate system ξ, ŋ, where the Oŋ axis is the front of the cascade (Fig. 1.8 and 1.11). Let ξ̄ 0 and ŋ 0 be the dimensionless coordinates defined in (7.51) for any point of the plane; then for the disturbed velocity at this point we have

$$\left. {{}_{{W_\eta }\left( {{{\bar \xi }_0},{{\bar \eta }_0}} \right) = \frac{1}{{2t}}\int {\gamma \left( s \right){w_\eta }\left( {{{\bar \zeta }_0} - \bar \zeta ,{{\bar \eta }_0} - \bar \eta } \right)ds,} }^{{W_{\bar \varsigma }}\left( {{{\bar \xi }_0},{{\bar \eta }_0}} \right) = \frac{1}{{2t}}\int {\gamma \left( s \right){w_\zeta }\left( {{{\bar \zeta }_0} - \bar \zeta ,{{\bar \eta }_0} - \bar \eta } \right)ds} }} \right\}$$
((8.1))

since the differential γ(s)ds will correspond in dimension to the circulation Γ+ of Eqs. (7.51). In (8.1), the integration is taken along the length of each profile and the expressions for w ξ and W η are given by Eqs. (7.50).

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© 1967 Springer Science+Business Media New York

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Belotserkovskii, S.M. (1967). Equations for Determination of the Strength of a Bound Vortex Sheet. In: The Theory of Thin Wings in Subsonic Flow. Springer, Boston, MA. https://doi.org/10.1007/978-1-4899-6299-7_8

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  • DOI: https://doi.org/10.1007/978-1-4899-6299-7_8

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4899-6161-7

  • Online ISBN: 978-1-4899-6299-7

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