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...

Full description

Saved in:
Bibliographic Details
Main Author: Zhao Xuan, Chang Sijiang, Ni Yi
Format: article
Language:ZH
Published: Editorial Office of Aero Weaponry 2021
Subjects:
Online Access:https://doaj.org/article/4b308f2369f740278cfa47d6d3046653
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items