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
of the large one, a contract was entered into on February 23, 1900,
which specified that the engine should be delivered by April 1, with
a penalty for any delay beyond that date.
The frame for this quarter-size model was immediately begun and
extra workmen were employed for work on it in order that its
construction should in no way delay the completion of the large
machine. The decision to construct this quarter-size model of the
large aerodrome had been made on the assumption that, since it was
to be one-sixteenth the weight of the large machine, and therefore
much heavier in comparison to its size than the steam models Nos. 5
and 6, it would, therefore, not need to be so carefully constructed
in order to obtain sufficient strength. But when construction was
actually begun it was found not only that the simpler and less
expensive methods which it had been proposed to use in joining its
frame together resulted in a weak construction, but also that the
time consumed in tinkering up the imperfections in the joints more
than counterbalanced the extra time which would have been required to
make the joints in the best manner from the beginning. Before going
very far it was therefore decided to make the joints by following
the same process which had been developed in the construction of
the previous models. The frame was accordingly built in the most
substantial manner, and when guyed by a system of guy-wires similar
to that employed for the large machine it was found to be exceedingly
stiff, in fact very much stronger and stiffer than the frame of any
of the preceding models.
In originally planning the model the intention was to make all its
linear dimensions exactly one-fourth those of the large aerodrome.
Before the designs were completed, however, it was seen from the
previous experience with the steam-driven models that instead of the
62.5-cm. propellers, which a strict adherence to the quarter-size
plan would demand, it would be necessary to use propellers which were
at least one metre in diameter. Moreover, as the small engine would
be more than one-fourth the size of the engine under construction
for the large aerodrome, a departure from the scale in the case of
the transverse frame would be necessary. The designs were therefore
altered so as to admit of using the larger propellers, and the tubes
which formed the front of the transverse frame were bent, as shown in
the plan photograph, Plate 70, in order to give a large enough space
for properly mounting the engine.
The frame with these modifications was completed in June, 1900, but
no engine was ready for it, as the builder had failed to fulfill
his contract for either the large or the small engine, although
several trips to New York had been made to expedite their successful
completion. [p228]
Public-domain text, read in full here on John Shaqi.
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