Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 188
Spreader Tubes Fig. 101 … 6 £5 lbs. Fig. 102 discusses the resiliency of elastic cord and its effect on the easy ridingqualities of a chassis. 122. Design of the Axle—Axles are calculated for the vertical loadin level landing, and are designed for a factor equal to or slightly lessthan the factor for the worse stressed…
Airplanes
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