An efficient multi-methods computer code for the prediction of the inviscid and viscous flow over multi-component airfoils

Author:

DE NICOLA C.1,COIRO D.2,LOSITO V.3

Affiliation:

1. Napoli, Universita, Naples, Italy

2. ItalianCentre for Aerospace Research, Naples, Italy

3. Academia Aeronautica, Pozzuoli, Italy

Publisher

American Institute of Aeronautics and Astronautics

Reference30 articles.

1. Evaluation of a stalled airfoil analysis program

2. A comparison of separated flow airfoil analysis methods

3. Amendola A., de Nicola C.,Losito V. & Vitiello D. ,1986, A Direct Method for Computing the Stall of Airfoils, Proc. VIII AIMETA Congress, Torino, Italy, pp.773-778.

4. Williams J.C.,1977, Incompressible Boundary Layer Separation, Annual Rewievs of Fluid

5. Numerical prediction of incompressible separation bubbles

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