2000 | OriginalPaper | Buchkapitel
Aeroelastic Analysis of a Helicopter Rotor in Forward Flight
verfasst von : B. Buchtala, K.-H. Hierholz, S. Wagner
Erschienen in: High Performance Computing in Science and Engineering ’99
Verlag: Springer Berlin Heidelberg
Enthalten in: Professional Book Archive
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Flow fields around rotary wings, especially around helicopter rotors, are extremely complex due to strong compressibility and three-dimensional effects. The solution of the governing equations for these flow problems is very difficult and can usually only be achieved with the help of numerical methods.