Abstract
SummaryThe incompressible planar flow past a wing with a jet issuing from the trailing edge is calculated by two separate methods, both adaptations of conformal mapping routines that are numerically exact in the jet-free case. These are the well-known circle mapping method and the halfplane method. The former is rendered inexact by the jump conditions across the jet and an approximation is necessary. The halfplane method, however, remains exact in principle, and a range of results is presented below. The most accurate of the previous calculations is verified, and comparisons between the halfplane and circle methods are also made. The halfplane scheme seems well suited for such wake-controlled flows and has been extended to transonic conditions in a related study.
Publisher
Cambridge University Press (CUP)
Reference20 articles.
1. Foster D.N. Note on methods of calculating the pressure distribution over the surface of Two-dimensional cambered wings. R.A.E. Technical Report 67095 (A.R.C. 29419), 1967.
2. Plane subcritical flow past a lifting aerofoil
3. Jameson A. Numerical calculation of the Three Dimensional Transonic Flow over a Yawed Wing. Proc. AIAA Computational Fluid Dynamics Conference, pp. 18–23, 1973.
4. Smith F.T. , and O’Mahoney R. Calculation of the transonic flow past an aerofoil and its wake. R.A.E. Technical Report 77037, 1977.
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