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Wind-tunnel investigation of effect of yaw on lateral-stability characteristics II Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics I Four N.A.C.A. 23012 wings of various plan forms with and without dihedral
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Wind-tunnel investigation of effect of yaw on lateral-stability characteristics
ID:
3436290
Creatori:
(1386953) Bamber, M. J.
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