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 method of measuring the final speed of the launching car for
the models consisted in fastening a strip of smoked paper to the
launching car in such a position that it was drawn past a stylus
fastened to the end of a vibrating tuning fork placed at the end
of the track. This had proved perfectly successful, but it gave a
record merely of the final speed attained by the car at the moment
of launching the aerodrome. In the case of the large aerodrome it
was desirable to have a record of the speed of the car during the
first few feet, and also at several other points in its travel down
the launching track, and the more numerous these points the better.
Short strips of copper were accordingly placed every twelve inches
along the length of the track, and these were connected by a wire
to one terminal of a small electric battery. Mounted on the car, in
such a way that it would be drawn across these contact strips, was a
copper brush arranged to make continuous contact with another wire
stretched along the track, this second wire being connected to the
other terminal of the electric battery and having in its circuit
the magnet which actuated a pen on a chronograph. Since the rate of
revolution of the chronograph barrel was known, the [p163] distance
between the marks which the magnet would cause the pen to make when
its circuit was closed by the brush on the car passing across the
contact strips on the track would give correct measures of the time
consumed by the car in passing over each twelve inches of its travel.
Upon test, however, it was found impossible to get the chronograph
magnets to work rapidly enough to respond to the very rapid opening
and closing of the circuit after the car had passed over the first
one-quarter of its length of travel. As a large part of the slowness
of action seemed to be due to the weight of the fountain pens, they
were replaced by small glass tubes drawn out to a fine point and
containing a small amount of ink. These seemed, however, to be still
too heavy to respond to the rapid closing of the circuit unless
the contacts were made unduly long. The contacts were finally made
three inches long and placed only every three feet along the track,
but just as these contacts were completed and placed in position
the clock-work of the chronograph itself became deranged. Before it
could be repaired, the tests were discontinued, as everything was in
readiness for the boat to proceed down the river where the actual
tests in free flight were to be made. Tests of the final speed of the
car were, however, made by the tuning-fork method, and the springs
were adjusted until their tension was sufficient to cause the car to
attain a speed of thirty-five feet a second at a point three inches
in front of the point at which the aerodrome would be released from
the car.
[p164]
CHAPTER V
CONSTRUCTION OF FRAME OF LARGE AERODROME
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