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(1923)

NASA Technical Reports Server (NTRS) · leaf 12

An illustration from , 1923, leaf 12
BENDING MOMENTS, ENVELOPE, AND CABLE STRESSES IN NON-RIGID AIRSHIPS. 13 By substituting the values of the quantities in this equation for each cable, the changes of tension are found to be as follows: In cable A, T= 180 pounds. In cable B, 7*= -342 pounds. In cable C, T= 750 pounds. In cable D, T=… … The tensions in cables A and B in the static condition are found from the force diagram in the accompanying figure to be 1,785 pounds and 1,190 pounds, respectively. The final tensions in the cables are: In cable A, tension «1,965 pounds. In cable B, tension = 848 pounds. In cable C, tension - 750…

NASA Technical Reports Server (NTRS)

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