Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911Langley, S. P. (Samuel Pierpont)
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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
In the second trial it repeated in nearly every respect
the action of the first, and with an identical result.
It rose smoothly in great curves until it approached a
prominent wooded promontory, which it crossed at a height
of 8 to 10 metres above the tops of the highest trees,
upon the exhaustion of the steam descending slowly into
the bay, where it settled in a minute and thirty-one
seconds from the start. You have an instantaneous
photograph of it, which I took just after the launch. [See
plates 20, 21, and 22 of present work.]
From the extent of the curves which it described, which
I estimated with other persons, from measurements which
I took, and from the number of revolutions of the
propellers, as recorded by the automatic counter which I
consulted, I estimate the absolute length of each course
to be over half an English mile, or, more exactly a little
over 900 metres (2953 feet).
The duration of flight during the second trial was one
minute and thirty-one seconds, and the average velocity
between twenty and twenty-five miles an hour, or, let us
say 10 metres a second, in a course which was constantly
ascending. I was extremely impressed by the easy regular
course of each trial, and by the fact that the apparatus
descended each time with such smoothness and gentleness as
to render any jar or danger out of the question.
It seemed to me that no one could have witnessed these
experiments without being convinced that the possibility
of mechanical flight had been demonstrated.
[8] It is desirable that the reader should be acquainted with the
contents of this treatise, and of another by me, entitled “The
Internal Work of the Wind,” both published by the Smithsonian
Institution. A knowledge of these works is not absolutely necessary,
but of advantage in connection with what follows.
[9] “Experiments in Aerodynamics,” p. 107.
[10] Chapter VIII.
[11] His device for obtaining automatic equilibrium is found in
connection with the description of his “Aeroplane Auto Moteur,” in
“L’Aeronaute” for January, 1872.
[12] I have never obtained so good a result as this with any rubber
motor. S. P. Langley.
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