Aerodynamics characteristics of a canard controlled high fineness ratio missile
Applied Aerodynamics Conference ; 1983 ; Danvers , MA , U.S.A.
01.01.1983
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aerodynamic Characteristics of a Canard-Controlled Missile at High Angles of Attack
Online Contents | 1994
|Aerodynamic Characteristics of a Canard-Controlled Missile with a Free-Spinning Tail
British Library Conference Proceedings | 1998
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