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Tables of stiffness and carry-over factor for structural members under axial load (1938)

NASA Technical Reports Server (NTRS) · leaf 4

An illustration from Tables of stiffness and carry-over factor for structural members under axial load, 1938, leaf 4
N.A.C.A. Technical Note No. 653 4 L L — csch — - 1 J J a = 6 … Effective values of a and (3 are obtained by substitu- tion of (L/j)eff for L/j . FORMULAS USED IF CALCULATION OF TABLES In tables I and II for compression and tension, re- spectively, the far end of the member is considered as either pinned or fixed. The stiffness and carry-over fac- tor that…

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