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 weight of the rubber in each tube was 72 grammes, or 0.16 pounds;
mean speed of flight in horizontal distance 4-1/2 metres (about 15
feet) per second.[16]
From experiments already referred to, there were found available
300 foot-pounds of energy in a pound of rubber as employed, and in
0.16 of a pound, 48 foot-pounds of energy were used; 48/33,000 or
0.00145 = the horse-power exerted in [p019] one minute, but as the
power was in fact expended in 1/20 of that time we have 20×0.00145 =
0.029; that is, during the brief flight, about 0.03 of a horse-power
was exerted, and this sustained a total weight of only about a pound.
In comparing this flight with the ideal conditions of horizontal
flight in “Aerodynamics,” it will be remembered that this model’s
flight was so irregular and so far from horizontal, that in one
case it flew up and struck the lofty ceiling. The angle with the
horizon is, of course, so variable as to be practically unknown, and
therefore no direct comparison can be instituted with the data given
on page 107 of “Experiments in Aerodynamics,” but we find from these
that at the lowest speed there given of about 35 feet per second,
0.03 of a horse-power exerted for three seconds would carry nearly
one pound through a distance of somewhat over 100 feet in horizontal
flight.
The number of turns of the propellers multiplied by the pitch
corresponds to a flight of about 16 metres, while the mean actual
flight was about 12. It is probable, however, that there was really
more slip than this part of the observation would indicate. It
was also observed that there seemed to be very little additional
compensatory gain in the steering of No. 30 for the weight of the
long rudder-tail it carried. It may be remarked that in subsequent
observations the superiority of the curved wing in lifting power
was confirmed, though it was found more liable to accident than
the flatter one, tending to turn the model over unless it was very
carefully adjusted.
It may also be observed that these and subsequent observations show,
as might have been anticipated, that as the motor power increased,
the necessary wing surface diminished, but that it was in general an
easier and more efficient employment of power to carry a surface of
four feet sustaining area to the pound than one of three, while one
of two feet to the pound was nearly the limit that could be used with
the rubber motor.[17]
It may be remarked that the flights this day, reckoned in horizontal
distance, were exceptionally short, but that the best flights at
other times obtained with these models (30 and 31) did not exceed
25 metres. Such observations were continued in hundreds of trials,
without any much more conclusive results. [p020]
Public-domain text, read in full here on John Shaqi.
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