Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing
Based on the CFD/CSD coupling method, the transonic static aeroelastic characteristics of the low-aspect-ratio swept wing was studied by numerical simulation. The Navier-Stokes equation was used as the fluid computational control equations. The flow field mesh deformation was performed using the Tra...
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| Format: | Article |
| Language: | English |
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AIP Publishing LLC
2019-04-01
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| Series: | AIP Advances |
| Online Access: | http://dx.doi.org/10.1063/1.5087963 |