The Effect of Tail Fin Parameters on the Induced Roll of a Canard Controlled Missile
28th, AIAA Applied Aerodynamics Conference ; 2010 ; Chicago, Il
01.01.2010
17 pages
Aufsatz (Konferenz)
Englisch
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Experimental Study of Tail-Span Effects on a Canard-Controlled Missile
Online Contents | 1993
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