A novel aerodynamic modeling method for an axisymmetric missile with tiny units

This article investigates the aerodynamic modeling problem of an axisymmetric missile with tiny units. Three aerodynamic force models for an axisymmetric air-to-air standard model missile are established. The mathematical model of trigonometric series model, response surface model, and kriging model...

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Bibliographic Details
Published in:Advances in Mechanical Engineering
Main Authors: Gong Chen, Zhigong Tang, Wenzheng Wang, Mingxin Xu
Format: Article
Language:English
Published: SAGE Publishing 2019-04-01
Online Access:https://doi.org/10.1177/1687814019839511