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
A brief account has already been given of the attempts made by Mr.
Langley to secure a suitable gasoline engine for the large aerodrome,
but the difficulties encountered in the search have not perhaps been
sufficiently emphasized. At this time (1898) the automobile industry,
through which has come the development of the gasoline engine, was
in its infancy, and there were few builders either in the United
States or Europe who were attempting anything but rough and heavy
construction. Many of them were enthusiastic over the possibilities
of the internal combustion engine, and were ready to talk of devising
such an engine as the aerodrome would require, but few were willing
to guarantee any such definite results as were demanded. However,
the prospects of securing a suitable gasoline engine from a reliable
builder within a reasonable time seemed so strong that it was decided
early in 1898 to begin the construction of the frame on the general
plan which would probably be best adapted for use with a gasoline
engine, and in case it finally proved impossible to secure such an
engine, to construct later a steam plant which could be adapted to
this particular frame.
Some tentative work on the construction of the frame was accordingly
begun in the summer of 1898, some months before an engine builder was
found who seemed likely to be successful in furnishing the engines.
An extensive series of tests on propellers was also made at this time
for the immediate purpose of determining what form and size would
be best, since the dimensions of the transverse frame could not be
definitely settled until it was known how large the propellers would
need to be.
Preliminary designs were also begun for the wings, rudders, and
launching apparatus, but when the point was reached of actually
making the working drawings for these, it was seen that the change
in the scale of the work required many important modifications in
constructional details. As the models had flown successfully only
three times, and in each case under practically the same conditions,
it was felt that it would be unwise to make changes in important
details without first making a series of tests of the models in
flight to determine the effect of such changes. It was therefore
decided to completely overhaul Models Nos. 5 and 6, strengthening
them in many important parts and “tuning up” their power plants,
which had slightly deteriorated since they were last used in
November, 1896. When the work of preparing these models for further
experiments was begun it was thought that it would require at most
only a few weeks, but as it progressed it was found that certain
parts of the mechanical work on the engines had been so poorly
executed originally that it would be necessary to practically rebuild
the engines. The final result was that the power plants of both
aerodromes were entirely rebuilt, and they were not ready for actual
test in flight until the spring of 1899. [p132]
Public-domain text, read in full here on John Shaqi.
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