Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911Langley, S. P. (Samuel Pierpont)
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Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911
Langley, S. P. (Samuel Pierpont)
Aeronautics; Flight
twisted, yet, after much training, the workmen were taught to twist
these very uniformly, following the plan which can be best understood
by an inspection of the drawings in Plate 55 which show the loops
more clearly than they can be described. After the loops had been
properly twisted, soft solder was run all through the twist in order
to unite firmly the twists of the wire. Although special grades of
wire were found which showed very high tensile strength when the wire
was [p172] tested without having loops formed in its ends, yet it
appeared that the twisting of these high-grade wires so seriously
affected them that in the case of guy-wires with loops at the ends,
better final results could be obtained by using softer grades of
steel. The wire which was actually found best, after much experiment,
was a good grade of Bessemer steel of a medium hardness, which had
been “coppered” to prevent rusting. However, even with the softer
grades of steel wire, it was found that there were sometimes hard
spots in the wire which revealed themselves only upon test, and that
when a hard spot occurred in the twisted portion where the loop was
formed, the final strength of the completed guy-wire was sometimes
only twenty-five per cent of what it should be. The precaution was
then taken to subject each of the completed guys to a test strain at
least twenty-five per cent greater than it was calculated the wire
would have to stand in actual use, so that no accident from defective
wires would be likely to occur.
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