Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 165
are investigated: cases I. 4, 6 and 7. II. The weight of the fully loaded airplane is 1650 lbs. III. The design of this chassis is such that in front elevationthere is no eccentricity of struts, wires or spreader tubes. In sideelevation, a slight eccentricity of struts and axle is present, aswell… … Art. 113
Airplanes
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