Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911 — John Shaqi
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 steam engine on a small scale, and under the actual restrictions
of the model, must necessarily be extremely wasteful of power. If we
suppose it to realize 2 per cent of the theoretical energy contained
in the fuel, we shall be assuming more than was actually obtained.
The energy of the fuel cannot be obtained at all, of course, without
boiler and engine, whose weight, for the purpose of the following
calculation, must be added to that of the fuel; and if we suppose
the weight of the boilers, engines and water, for a single minute’s
flight, to be collectively ten pounds, we shall take an optimistic
view of what may be expected under ordinary conditions. We have
in this view 1/500 of the [p025] theoretical capacity possibly
realizable under such conditions, but if we take 1/1000 we shall
probably be nearer the mark. Even in this case we have, when using
gasoline as fuel, 15,625 foot-pounds per minute, or nearly 0.50
horse-power, as against .0091 horse-power in the case of the rubber,
so that even with this waste and with the weight of the engines
necessary for a single minute’s service, the unit weight of fuel
employed in the steam engine gives 55 times the result we get with
rubber.
[Illustration: PL. 5
RUBBER-PULL MODEL AERODROME]
[Illustration: PL. 6
RUBBER-PULL MODEL AERODROME]
[Illustration: PL. 7
RUBBER-PULL MODEL AERODROME]
[Illustration: PL. 8
RUBBER-PULL MODEL AERODROME]
[Illustration: PL. 9
RUBBER-PULL MODEL AERODROME]
With alcohol we have about 2/3 the result that is furnished by
gasoline, since nearly the same boiler and engine will be used
in either case. Certain difficulties which at first appeared to
be attendant on the use of gasoline on a small scale induced me
to make the initial experiments with alcohol. This was continued
because of its convenience during a considerable time, but it was
finally displaced in favor of gasoline, not so much on account of
the superior theoretical efficiency of the latter, as for certain
practical advantages, such as its maintaining its flame while exposed
to wind, and like considerations.
GUNPOWDER
Although there are other explosives possessing a much greater energy
in proportion to their weight than gunpowder, this is the only one
which could be considered in relation to the present work, and the
conclusion was finally reached that it involved so great a weight
in the containing apparatus and so much experiment, that, although
the simplicity of its action is in its favor where crude means are
necessary, experiments with it had better be deferred until other
things had been tried.
HOT-WATER ENGINE
A great deal of attention was given to the hot-water engine, but it
was never put to practical use in the construction of an aerodrome,
partly on account of the necessary weight of a sufficiently strong
containing vessel.
COMPRESSED AIR
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