Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911Langley, S. P. (Samuel Pierpont)
History
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
Experience, both with models 5 and 6, and with the quarter-size
model, had also demonstrated the necessity of providing some means
whereby the aerodrome frame would be relieved of the torsional
strains produced upon it by a side wind striking the under surface of
the wings when the aerodrome was mounted on the car preparatory to a
test. The means for preventing these torsional strains in the case of
the models, when “overhead” type of launching car was used, has been
described in Chapter X of Part I. However, with the “underneath” type
of launching car, a different means was necessary. A plan, in which
outriggers projected from the body of the car and wires running from
these outriggers up to the main ribs of the wings, with means for
releasing the wires just before the car reached the end of the track,
was used with the “underneath” car in the tests of models 5 and 6 in
the summer of 1899, but the outriggers were frequently deranged by
the sudden stopping of the car at the end of the run and they were
replaced by a simpler arrangement. In this plan the torsional strains
were relieved by providing, at the forward and rear ends [p159] of
the car, smaller hinged uprights furnished in their upper part with a
small slot into which a pin projected from the bottom of the forward
and rear guy-posts, respectively. The guy-wires from wings being
connected to the lower ends of the guy-posts the torsional strain
produced by a side wind was immediately transmitted from the wings
through the guy-wires to the guy-post, whence it was transmitted to
the car itself, and thus prevented from acting on the metal frame of
the aerodrome, as shown in Plate 39. These additional short struts
for taking up the torsional strain were first added to the small
launching car in 1901, and in the succeeding tests made with the
quarter-size model no trouble of any kind was indicated as likely to
be caused by them. As it was these extra struts which were directly
responsible for the accident in the launching of the large aerodrome
October 7, 1903, at the time of its first trial, and possibly also
for that on December 8, 1903, at the time of the second trial,
special attention is here called to them.
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