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The Vortex lattice method, (VLM), is a numerical method used in computational fluid dynamics, mainly in the early stages of aircraft design and in aerodynamic education at university level. The VLM models the lifting surfaces, such as a wing, of an aircraft as an infinitely thin sheet of discrete vortices to compute lift and induced drag. The influence…
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Vortex lattice method | related to Assumptions | The | 0.60 | section |
| Vortex lattice method | related to Assumptions | However | 0.60 | section |
| Vortex lattice method | related to Assumptions | Prandtl-Glauert | 0.60 | section |
| Vortex lattice method | related to Extension to the Dynamic Case | The | 0.60 | section |
| Vortex lattice method | related to Extension to the Dynamic Case | Commonly | 0.60 | section |
| Vortex lattice method | related to Extension to the Dynamic Case | Doublet Lattice Method | 0.60 | section |
| Vortex lattice method | related to Extension to the Dynamic Case | Each | 0.60 | section |
| Vortex lattice method | related to Extension to the Dynamic Case | The Doublet Lattice Method | 0.60 | section |
| Vortex lattice method | related to Extension to the Dynamic Case | Vortex Lattice | 0.60 | section |
| Vortex lattice method | related to Theory | The | 0.60 | section |
| Vortex lattice method | related to Theory | Potential | 0.60 | section |
| Vortex lattice method | related to Theory | Ideal | 0.60 | section |
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