Landing gear noise prediction using high-order finite difference schemes
Aerodynamic noise from a generic two-wheel landing-gear model is predicted by a CFD/FW-H hybrid approach. The unsteady flow-field is computed using a compressible Navier-Stokes solver based on high-order finite difference schemes and a fully structured grid. The calculated time history of the surfac...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
2013-07-08.
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| Subjects: | |
| Online Access: | Get fulltext |