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
1923-12-01
Miscellaneous
No indication
English
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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