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
The terminal
which passed through the insulator was also extended for something
like half an inch beyond the porcelain and bent to a proper extent
to co-act with a piece of platinum wire inserted in the interior
wall of the plug which formed the other terminal. After making this
improvement in the plugs practically no difficulty was experienced
from short-circuits caused by the soot.
In making the tests of this experimental engine it was found
practically impossible to absorb the power by a Prony brake in a
sufficiently uniform manner on account of the fact that the engine
was being run without a fly wheel. The consequent variation in
the torque and speed during each revolution caused such great
fluctuations in the reading of the scales which measured the pull of
the Prony brake that no confidence could be felt in the accuracy of
the readings and, therefore, no confidence could be placed in the
determinations of the effect which different changes in the engine
produced. A water-absorption dynamometer consisting of a number
of flat, circular discs fastened to a shaft and rotating between
other parallel flat discs arranged in a circular drum which was
filled to any desired extent with water was immediately planned,
and the construction of two of them was begun so that power could
be taken from both ends of the engine shaft, which, on account of
its necessary lightness, was apt to be injured by being twisted
when all the power was taken from one end of the shaft. In order to
continue the tests on the engine while this dynamometer was being
made it was decided to employ one of the propellers as a dynamometer.
Although no accurate tests had been made to determine just how much
power was required to drive these propellers at various speeds, yet
the fundamental law was known that under the same conditions the
power required to drive any propeller would vary as the cube of the
number of revolutions, and since the Prony-brake tests had given an
approximation as to the amount of power which the engine developed at
certain speeds, the law of the propeller, and extrapolations from the
data obtained in the tests of the smaller propellers in 1898, enabled
further approximations to be made as to the amount of extra power
which the engine developed when certain changes enabled it to drive
the propeller at increased speeds. This method had also the great
advantage that, since the power required varies as the cube of the
number of revolutions, it is practically impossible for the engine to
“run away” with the propeller and cause serious damage through the
possible excessive strains introduced by high speed. This feature is
also possessed by water-absorption dynamometers of the type which
were built and used in the later tests.
Public-domain text, read in full here on John Shaqi.
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