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Air force and three moments for F-5-L Seaplane (1922) (14578842308)
Summary
Identifier: nasa_techdoc_19930080857 (find matches)
Title: Air force and three moments for F-5-L Seaplane
Year: 1922 (1920s)
Authors: NON
Subjects:
Publisher:
Contributing Library: NASA
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Text Appearing Before Image:
xo>n j-jii.^ diAJJO of j^ull-^iae ^eaplanelongitudinal axis to edges; euA.xt Angle of yaw.Fig, 5. Yawing moments -with hull yawed and rudder neutral to hull. Wind speed M-0 m.p,h.
Text Appearing After Image:
Deflection of aileron from wing chord.Fig. 6. Rolling moment at various positions of ailerons. Axis of hull parallel to wind. Wind speed ^0 m.p.h.
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