Two different wing configurations considered; for cruciform winged missile it is shown that regions of unstable controllability can exist when tail planes are rotated over 45° with respect to wings; as to annular wing configuration it is noted that, due to interference effects, favorable drag characteristics can be obtained for combination as whole.
Aerodynamic aspects of design of guided missiles and rockets
Aerodynamische aspecten bij het ontwerp van geleide projectielen en raketten
Ingenieur ; 71 , n 39
1959
Article (Journal)
Dutch
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