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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