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JOURNALS // Zhurnal Vychislitel'noi Matematiki i Matematicheskoi Fiziki // Archive

Zh. Vychisl. Mat. Mat. Fiz., 2014 Volume 54, Number 8, Pages 1281–1288 (Mi zvmmf10075)

This article is cited in 1 paper

Two methods for direct numerical integration of the Prandtl equation and comparative analysis between them

A. V. Sahakyana, N. N. Shavlakadzeb

a Institute of Mechanics, National Academy of Sciences of Armenia, pr. Marshala Bagramyana 24b, Yerevan, 0019, Armenia
b A. Razmadze Mathematical Institute, Georgian Academy of Sciences

Abstract: Two methods based on quadrature formulas are proposed for the direct numerical integration of Prandtl’s singular integro-differential equation. In the first method, Prandtl’s equation is solved directly by applying the method of mechanical quadrature and the circulation along an airfoil section is determined. In the second method, Prandtl’s equation is rewritten for the circulation derivative, which is determined by applying mechanical quadratures, and the circulation is then reconstructed using the same quadrature formulas. Both methods are analyzed numerically and are shown to converge. Their convergence rates are nearly identical, while the second method requires much more CPU time than the first one.

Key words: finite wing theory, Prandtl’s singular integro-differential equation, complex wing geometry, numerical integration, method of mechanical quadrature.

UDC: 519.642

MSC: 76F40

Received: 23.09.2013
Revised: 21.01.2014

DOI: 10.7868/S0044466914080134


 English version:
Computational Mathematics and Mathematical Physics, 2014, 54:8, 1244–1250

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