Hybrid solver for aerodynamic design
Hybrid solver for aerodynamic design
Date
2020
Authors
Nikolsky, A.
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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