Analysis of flight and wind-tunnel tests on Udet airplanes with reference to spinning characteristics (1929)
NASA Technical Reports Server (NTRS) · leaf 24
.A.C.A. Technical Hemorandum No•502 CV3 Fig.3 … •6900 nmi Jji^^j -^^|-^10 X 85 mm 1600- ■100 imn r""^-m^^^^ 2612^^ r^r^ - -1200 mm —J (^j-—f ir r3012 1340" mm ^^^^ Fig.3 U12 Flamingo biplane.80 HF Siemens.2 seats.The lengthened fusela.ge and enlarged vertica,l fins o;nd rudders used, on the wind tunnel model are shown in dotted lines.
NASA Technical Reports Server (NTRS)
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