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.
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.