Research on the Rapid Aerodynamic Shape Optimization of Canards of Gliding Guided Projectile

In order to improve the accuracy of calculation, it is often necessary to calculate the aerodynamic parameters of the projectile iteratively through computational fluid dynamics simulation, so the optimization efficiency is low. In this paper, a rapid aerodynamic shape ptimization method based on mu...

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Auteur principal: Zhao Xuan, Chang Sijiang, Ni Yi
Format: article
Langue:ZH
Publié: Editorial Office of Aero Weaponry 2021
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Accès en ligne:https://doaj.org/article/4b308f2369f740278cfa47d6d3046653
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