Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 174
he struts is inversely proportional to theirlength and directly proportional to their moment of inertia. Owing to the rigid connection of the struts and spreader tubes to theguide plate, any moment in a vertical plane perpendicular to the planeof the struts cannot be concentrated in the struts on… … / 00Externa/ Moment Fig. 97 155 Airplane Chassis Art. 117 Sum of maximum moments in struts on right sidems = mf -\- mrmc = Moment in spreader tubes = 1.00—ms = m£l + mn — Sum of maximum moments in the struts on the left side. As the front and rear struts are the same size, the moment taken byeach…
Airplanes
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