Comparative accuracy and performance assessment of the finite point method in compressible flow problems

Other authors

Escola Tècnica Superior d'Enginyeries Industrial i Aeronàutica de Terrassa

Universitat Politècnica de Catalunya. Departament de Resistència de Materials i Estructures a l'Enginyeria

Centre Internacional de Mètodes Numèrics en Enginyeria

Universitat Politècnica de Catalunya. (MC)2 - Grup de Mecànica Computacional en Medis Continus

Universitat Politècnica de Catalunya. L'AIRE - Laboratori Aeronàutic i Industrial de Recerca i Estudis

Publication date

2014-01-20

Abstract

A comparative assessment of the Finite Point Method (FPM) is presented. Using a wing-fuselage configuration under transonic inviscid flow conditions as reference test case, the performance of the FPM flow solver is compared with an equivalent edge-based Finite Element (FEM) implementation. Efficiency issues have discouraged practical application of meshless methods in the past. Thus, a simplification of the basic FPM technique is proposed in order to reduce the performance gap with respect to classical grid-based algorithms. A comparative evaluation of the accuracy, computational cost and parallel performance of the meshless implementation is carried out with the objective to assess the level of maturity of the technique and identify improvements still required to tackle practical applications. The results obtained show accuracy and performance of the core algorithm comparable to a conventional FEM implementation, thus removing a major obstacle for further developments of the FPM.


Peer Reviewed


Postprint (published version)

Document Type

Article

Language

English

Publisher

Elsevier

Related items

http://www.sciencedirect.com/science/article/pii/S0045793013004076

info:eu-repo/grantAgreement/EC/FP7/211785/EU/Aerodynamic loads estimation at extremes of the flight envelope/ALEF

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E-prints [72987]