Hybrid solver for aerodynamic design
| dc.contributor.author | Nikolsky, A. | |
| dc.date.accessioned | 2024-04-17T10:38:32Z | |
| dc.date.available | 2024-04-17T10:38:32Z | |
| dc.date.issued | 2020 | |
| dc.description.abstract | The low-fidelity generalized inverse solver is developed. It allows to control the pitching moment when the original pressure distribution is corrected. The new hybrid method of aerodynamic design is stated. It uses the generalized inverse solver as a geometry parameterizer along with the solvers of any fidelity to evaluate the objective function | |
| dc.identifier.other | 1346 erf2020 | |
| dc.identifier.uri | https://hdl.handle.net/20.500.11881/4170 | |
| dc.language.iso | en | |
| dc.title | Hybrid solver for aerodynamic design |
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