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
Files
Categories
Aircraft Aerodynamics, Cooperative Control, Missile Dynamics