Flow near the Apex of a Plane Delta Wing
- 1 June 1969
- journal article
- Published by Oxford University Press (OUP) in IMA Journal of Applied Mathematics
- Vol. 5 (2) , 206-216
- https://doi.org/10.1093/imamat/5.2.206
Abstract
A series expansion is obtained for the exponent n of the singularity of the solution of Laplace's equation for the flow near the apex of a plane delta wing when the angular sector occupied by the wing is small. A further term is found in the expansion due to Legendre when the wing is almost a half-plane, and the value of n is determined numerically for a range of intermediate values of the apex angle.Keywords
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