Unsteady inviscid flowfields of 2D airfoils by non-linear singular integral computational analysis

Author:

Ladopoulos E.G.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference26 articles.

1. A.M.O. Smith, J.L. Hess, Calculation of the non-lifting potential flow about arbitrary three dimensional bodies, Douglas Report E.S. 40622, 1967.

2. A numerical method for the calculation of non-linear unsteady lifting potential flow problems;Djojodihardjo;AIAA J.,1969

3. P.E. Robert, G.R. Saaris, Review and Evaluation of a Three-Dimensional Lifting Potential Flow Computational Method for Arbitrary Configurations, Boeing Co., 1972.

4. Potential flow about impulsively started rotors;Summa;J. Aircraft,1976

5. D.R. Bristow, Development of Panel Methods for Subsonic Analysis and Design, NASA CR–3234, 1980.

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1. Effective Prediction of Coefficients and Performance of Airfoil Using ANN;2024 Fourth International Conference on Advances in Electrical, Computing, Communication and Sustainable Technologies (ICAECT);2024-01-11

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