Compressive Strength of Tapered Airplane Struts (open access)

Compressive Strength of Tapered Airplane Struts

Note presenting methods for ascertaining the value of n in Euler's simplified formula, which can be used for the compressive strength of tapered airplane struts, by estimating from curves and by calculation.
Date: December 1923
Creator: Lewe, Viktor
System: The UNT Digital Library