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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

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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.

Metadaten
Titel
Aeroelastic Analysis of a Helicopter Rotor in Forward Flight
verfasst von
B. Buchtala
K.-H. Hierholz
S. Wagner
Copyright-Jahr
2000
Verlag
Springer Berlin Heidelberg
DOI
https://doi.org/10.1007/978-3-642-59686-5_29