Methods are here given for ascertaining the value of n in Euler's simplified formula, P = n (EI/l(sup 2)), for the compressive strength of tapered airplane struts, by estimating from curves and by calculation.
Compressive Strength of Tapered Airplane Struts
01.12.1923
Sonstige
Keine Angabe
Englisch
Compressive strength of tapered airplane struts
Engineering Index Backfile | 1923
|Engineering Index Backfile | 1919
|Remarks on airplane struts and girders under compressive and bending stresses. index values
Engineering Index Backfile | 1929
|Effect of end fixation of airplane struts
Engineering Index Backfile | 1930
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