Aeroelastic Analysis of a Helicopter Rotor in Forward Flight

B. Buchtala, K.-H. Hierholz and S. Wagner
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B. Buchtala: Universität Stuttgart, Institut für Aerodynamik und Gasdynamik
K.-H. Hierholz: Universität Stuttgart, Institut für Aerodynamik und Gasdynamik
S. Wagner: Universität Stuttgart, Institut für Aerodynamik und Gasdynamik

A chapter in High Performance Computing in Science and Engineering ’99, 2000, pp 327-330 from Springer

Abstract: Abstract 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.

Keywords: Helicopter Rotor; Forward Flight; Approximate Riemann Solver; Background Grid; Rotary Wing (search for similar items in EconPapers)
Date: 2000
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-642-59686-5_29

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DOI: 10.1007/978-3-642-59686-5_29

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