Aerodynamic performance improvement of a canard control missile
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DOI: 10.1108/aeat-01-2016-0019
Abstract: Purpose This paper aims to analyze the influence of the changings in geometrical parameters on the aerodynamic performance of the control canard projectiles. Design/methodology/approach Because of the mentioned point, the range of projectiles increment has… read more here.
Keywords: taper ratio; control; ratio; lift drag ... See more keywords