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Analysis of flight and wind-tunnel tests on Udet airplanes with reference to spinning characteristics (1929)

NASA Technical Reports Server (NTRS) · leaf 22

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Technical Kemorandum Ho.b02 Fig.l H CV3 … 745-, (-400 mm 740-^ , . 400 4|-r3,^_.950 ^200 mm 1300 mm 5364 mm-^ .1 U6. Low TTing monoplane.60 HP Siemens.2 seats.

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