Three-dimensional oscillatory piecewise continuous-kernel function method-part II: Geometrically continuous wings

I. Lottati, E. Nissim

Research output: Contribution to journalArticlepeer-review

Abstract

The rapid convergence and high-accuracy characteristics of the three-dimensional piecewise continuous-kernel function method (PCKFM) are tested in the present work. The large number of numerical examples which are included herein is aimed at showing the computational efficiency of the method. Three-dimensional wings with no geometrical discontinuities along their spans (discontinuities are permitted at the wing root only) are treated. Problems associated with geometrical discontinuities (such as break points, control surfaces, etc.) are presented in Part HI of this work.

Original languageEnglish
Pages (from-to)352-355
Number of pages4
JournalJournal of Aircraft
Volume18
Issue number5
DOIs
StatePublished - May 1981
Externally publishedYes

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