Journal of Applied Mathematics and Mechanics (about journal) Journal of Applied
Mathematics and Mechanics

Russian Academy of Sciences
 Founded
in January 1936
(Translated from 1958)
Issued 6 times a year
ISSN 0021-8928
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IssuesArchive of Issues2012-1pp.103-109

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S.A. Takovitskii, "The optimal conical twist of a delta wing," J. Appl. Math. Mech. 76 (1), 103-109 (2012)
Year 2012 Volume 76 Issue 1 Pages 103-109
Title The optimal conical twist of a delta wing
Author(s) S.A. Takovitskii (Zhukovskii, Russia, c.a.t@tsagi.ru)
Abstract The problem of reducing the drag of a wing at a specified lift in a supersonic flow is investigated. A solution for a delta wing is obtained in a simplified formulation of the optimization problem and a theoretical analysis. It is shown that the optimal conical wing is formed by elements of elliptical cones and planes. Numerical modelling of the flow of a non-viscous non-heat-conducting gas past the wing is performed, and the results of the theoretical analysis and direct optimization are compared.
Received 07 September 2010
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