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TsAGI Science Journal

ISSN Печать: 1948-2590
ISSN Онлайн: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2013007253
pages 775-786

GENERALIZED INVERSE AIRFOIL PROBLEM

Alexander Alexandrovich Nikolsky
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia

Краткое описание

The problem of airfoil design based on a given pressure distribution and pitching moment at zero lift is solved for the general case of potential flows. The solution is obtained in quadratures for incompressible fluid flow. Algorithms for the solution and numerical technique are developed for compressible flows, including transonic flows. An example of solving the generalized inverse problem in helicopter airfoil design is considered. The practical applicability of the method is verified by computational fluid dynamics Reynolds-averaged Navier−Stokes calculations.

Ключевые слова: airfoil, inverse problem

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