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EnglishUnsteady turbulent transonic flows over oscillating airfoils are investigated by using a novel third-order accurate scheme on block-structured meshes. Two turbulence models ( algebraic and two-transport equation models) are studied in order to generate flow fields in agreement with experimental data. Numerical results are presented for 2-D problems related to helicopter rotors in forward flight, including shock-stall phenomena. The advantages of using a high-order accurate method and a suitable turbulence model for this kind of applications are demonstrated.
| Titolo: | Accurate simulation of turbulent transonic flows over oscillating airfoils | |
| Autori: | ||
| Data di pubblicazione: | 1998 | |
| Abstract: | Unsteady turbulent transonic flows over oscillating airfoils are investigated by using a novel third-order accurate scheme on block-structured meshes. Two turbulence models ( algebraic and two-transport equation models) are studied in order to generate flow fields in agreement with experimental data. Numerical results are presented for 2-D problems related to helicopter rotors in forward flight, including shock-stall phenomena. The advantages of using a high-order accurate method and a suitable turbulence model for this kind of applications are demonstrated. | |
| Handle: | http://hdl.handle.net/11587/112526 | |
| ISBN: | 0471985791 | |
| Appare nelle tipologie: | Capitolo di Libro |
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