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
From this description of its action, it will be seen that the Pénaud
tail has the disadvantage of giving an undulatory flight, if the tail
is made rigid. This objection, however, can be easily overcome by
giving to it a certain amount of elasticity. It does not appear that
Pénaud gave much attention to this feature, but stress is laid upon
it in the article “Flight,” in the ninth edition of the Encyclopædia
Britannica, and I have introduced a simple device for securing it.
The complete success of the device implies a strictly uniform
velocity and other conditions which cannot well he fulfilled in
practice. Nevertheless, it is as efficient a contrivance for its
object as has yet been obtained.
More elaborate devices have been proposed, and a number of them,
depending for their efficiency upon the action of a variety of
forces, have been constructed by the writer, one of which will be
described later. This has the advantage that it tends to secure
absolutely horizontal flight, but it is much inferior in simplicity
to the Pénaud tail.
Apart from considerations about the thrust, the ‹CP› is in practice
always almost directly over the ‹CG›, and this relationship is,
according to what has been suggested, obtained by moving the
supporting surfaces relatively to the ‹CG›, or ‹vice versa›,
remembering, however, that, as these surfaces have weight, any
movement of them alters the ‹CG› of the whole, so that successive
readjustments may be needed. The adjustment is further complicated
by another important consideration, namely, that those parts which
‹change› their weight during flight (like the water and the fuel)
must be kept very near the ‹CG›. As the water and fuel tanks are
fixed, it appears, then, that the center of gravity of the whole is
practically fixed also, and this consideration makes the adjustment a
much more difficult problem than it would be otherwise.[25]
[Illustration: PL. 11
STEEL FRAMES OF AERODROMES NOS. 4, 5, 6. 1893, 1895 AND 1896]
[p053]
CHAPTER VII
HISTORY OF CONSTRUCTION OF FRAME AND ENGINES OF AERODROMES
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