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
two stop-watches, was one minute and forty-five seconds. The number
of revolutions of the propellers was 2801, or at the rate of 1600
R. P. M., which, with an allowance of fifty per cent slip, should
have carried the aerodrome a distance of 4600 feet in one and
three-quarter minutes. While the distance from the house-boat in a
straight line to the point at which the aerodrome descended was only
about 1600 feet, yet it was estimated by those present that this
straight-line distance was certainly not greater than one-third the
total length of the path traversed, which would mean a distance of
something like 4800 feet. The length of the course, as plotted on
the coast-survey map and afterwards measured, was 4200 feet, and it,
therefore, seemed safe to say that the total distance travelled was
about three-quarters of a mile, and the speed was, therefore, about
thirty miles an hour.
[p110]
CHAPTER X
DESCRIPTION OF THE LAUNCHING APPARATUS AND OF
AERODROMES Nos. 5 AND 6
Reference has already been made to the development of the “cast-off”
apparatus that was used at Quantico for launching the aerodrome. An
initial velocity is indispensable, and after long experiment with
other forms which proved failures, an apparatus was designed by me,
which gave a sufficient linear velocity in any direction. It had,
moreover, been found that, when the aerodrome was attached to any
apparatus upon the roof of the house-boat, such slight changes in
the direction and intensity of the wind as would ordinarily pass
unperceived, would tend to distort or loosen it from its support,
so that only the most rigid of fastenings at three independent
bearing points were of any use in holding it, while the wings must
be separately fastened down, lest they should be torn from their
sockets. It was, then, necessary to be able to fasten the aerodrome
very firmly to the cast-off apparatus, to start it upon its journey
in any direction with an initial linear velocity that should equal
its soaring speed, and to release it simultaneously at all points at
the very same instant, while at the same time the points of contact
of the launching device, to which it had just been fastened, were
themselves drawn up out of the way of the passing propellers and guys.
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