Computational fluid dynamics (CFD) data for a proposed Skid-to-Turn (STT) missile

Published: 2 October 2019| Version 1 | DOI: 10.17632/r7rjbf47dg.1
Contributor:
xingguang xu

Description

The proposed cruciform-fin STT missile can cruise at trimmed conditions. One can obtain the detailed data associated with the aerodynamic coefficients, and local aerodynamics can be obtained through linear interpolation.One can obtain the aerodynamic con

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Categories

Aircraft Aerodynamics, Cooperative Control, Missile Dynamics

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