Computational Analysis of a Model Scale Helicopter Rotor in Ground Effect

2017-09-22
In this study, a numerical investigation of ground effect of a helicopter rotor is investigated with Computational Fluid Dynamics method. For this purpose, a model scale 2 bladed helicopter rotor is chosen. An experimental study is referred for comparison and validity of CFD method.

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Citation Formats
M. Şahbaz, N. Sezer Uzol, and D. F. Kurtuluş, “Computational Analysis of a Model Scale Helicopter Rotor in Ground Effect,” presented at the AIAC-International Aerospace Conference, (20 - 22 Eylül 2017), Ankara, Türkiye, 2017, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/75328.