Analysis of wings with flow separation

Tuncer Cebeci, D. SEDLOCK, Ke‐Vin Chang, R. W. Clark

Journal of Aircraft · 1989 · 41 citations · 11 references

Concepts

Abstract

An interactive viscous/inviscid procedure has been developed combining a three-dimensional panel method with an inverse finite-difference boundary-layer method. The scheme incorporates both a two-dimensional and a quasi-three-dimensional boundary-layer scheme. The resulting method has been applied to the calculation of the flow over three-dimensional wings and wing/body configurations and it has been shown that the procedure can compute flows with significant regions of boundary-layer separation.

References

11