2005 | OriginalPaper | Buchkapitel
Companion Computer Programs
verfasst von : Tuncer Cebeci, Max Platzer, Hsun Chen, Kuo-Cheng Chang, Jian P. Shao
Erschienen in: Analysis of Low-Speed Unsteady Airfoil Flows
Verlag: Springer Berlin Heidelberg
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In this chapter we describe two computer programs. The computer program of Section 10.2 is for steady airfoil flows based on the Hess-Smith panel method (HSPM). The computer program in Section 10.3 is based on the interactive boundary layer method discussed in Chapters 4 and 5 and is applicable to both steady and unsteady laminar and turbulent flows, including separation. Several sample calculations for steady and unsteady airfoils are also presented. Both computer programs arc given on the accompanying CD-ROM.