Abstract
In the IDIHOM Project three aeroelastic testcases have been calculated. Two of them - LANN Wing and DLR-F6 wing-body configuration - have been conducted by PUT. The last one, the HART II rotor has been prepared by NLR. Each partner has used different technology and software tools, hence each of the testcases describes the results of the simulation and technology which has been used.
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Kotecki, K. et al. (2015). Aeroelastic Testcases in IDIHOM Project. In: Kroll, N., Hirsch, C., Bassi, F., Johnston, C., Hillewaert, K. (eds) IDIHOM: Industrialization of High-Order Methods - A Top-Down Approach. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 128. Springer, Cham. https://doi.org/10.1007/978-3-319-12886-3_28
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DOI: https://doi.org/10.1007/978-3-319-12886-3_28
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-12885-6
Online ISBN: 978-3-319-12886-3
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