Numerical Predictions of Tip Shape Effect on Helicopter Rotor Noise in Forward Flight
The effect of helicopter rotor blade tip shape on overall aircraft noise level is analyzed, in forward flight conditions. The infamous HART-II experimental data is used as a base for validations. Commercially available CFD software Ansys/Fluent is used to model the flow field over rotor-body interac...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Turkish Air Force Academy
2024-07-01
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| Series: | Havacılık ve Uzay Teknolojileri Dergisi |
| Subjects: | |
| Online Access: | https://jast.hho.msu.edu.tr/index.php/JAST/article/view/602/413 |