Free streamline-boundary layer analysis for separated flow over an airfoil

Author:

Bassanini Piero,Elcrat Alan

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,General Physics and Astronomy,General Mathematics

Reference24 articles.

1. L. Prandtl, inVerhandlungen des dritten internationalen Mathematiker-Kongress, Heidelberg 1904, Leipzig 1905, pp. 484?491.

2. H. Schlichting,Boundary Layer Theory, McGraw-Hill, New York 1968.

3. J. Moran,An Introduction to Theoretical and Computational Aerodynamics, Wiley, New York 1984.

4. B. Glimer and D. Bristow,Analysis of stalled airfoils by simultaneous perturbations to viscous and inviscid equations, AIAA J.20, 1160?1166 (1982).

5. B. Maskew and F. Dvorak,The prediction of C max using a separated flow model, J. American Helicopter Soc.23, 2?9 (1978).

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1. Arclength numerical continuation in free-boundary flow;Applied Mathematics and Computation;2014-03

2. Computation of the Helmholtz–Kirchhoff and reentrant jet flows using Fourier series;Applied Mathematics and Computation;2005-04

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