Aerodynamic needle optimization using pSeven and FloEFD software package (in English)

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Авторы:

Saratov A.A., Aksenov L.A., Khominich D.S.

Издание:

13th International Conference “AVIATION AND COSMONAUTICS — 2014”, p. 182-183

Абстракт:

The goal of the present work is do define an optimal geometry of aerodynamic needle within the required range of parameters in order to minimize supersonic drag at the different angles of attack.

Ключевые слова: Surrogate-based optimization, CFD analysis

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