A flight investigation of the effect of mass distribution and control setting on the spinning of the XN2Y-1 airplane (1935)
NASA Technical Reports Server (NTRS) · leaf 1
of iner- Control deflection^: Chord 45in. tia of Ailerons up . . 25* propel- Stagger 22- down. 15° Gap'at center 54 « Rudder . .:. . ±41° ler: Z£0 Incidence, upper wing .... 0" slug ft? Elevator up . . 25° 30' lower » 1° down . 29° 30' Fin offset ... _ 3° 25" Dihedral, upper ■■ 0° lower » ..... 4°… … a. Ballast containers, a Clark Y 15% thick, e. Base line. m. £ Hinge. Fiooke 1.—Line drawing and general dimensions of the XN2Y-1 airplane. for frequent changes of the damping oil with changes RESULTS of air temperature. Special precautions were also Before presenting the results of the tests, a…
NASA Technical Reports Server (NTRS)
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