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
It is inevitable that in so complex a study some repetition should
present itself, especially in the narrative form chosen as the
best method of presenting the subject to the reader. Each of these
chapters, then, will contain its own historical account of its own
theme, so that each subject can be pursued continuously in the order
of its actual development, while, since they were all interdependent
and were actually going on simultaneously, the order of dates which
is followed in each chapter will be a simple and sufficient method of
reference from one to the other.
EXPERIMENTS WITH SMALL MODELS
In order to understand how the need arises for such experiments in
fixing conditions which it might appear were already determined in
the work “Experiments in Aerodynamics,”[8] it is to be constantly
borne in mind, as a consideration of the first importance, that the
latter experiments, being conducted with the whirling-table, force
the model to move in horizontal flight and at a constant angle. Now
these are ideal conditions, as they avoid such practical difficulties
as maintaining equilibrium and horizontality, and for this reason
alone give results more favorable than are to be expected in free
flight.
Besides this, the values given in “Aerodynamics” were obtained
with rigid surfaces, and these surfaces themselves were small and
therefore manageable, while larger surfaces, such as are used in
actual flight, would need to be stiffened by guys and like means,
which offer resistance to the air and still further reduce the
results obtained. It is, therefore, fairly certain, that nothing
like the lift of 200 pounds to the horse-power for a rate of 40
miles an hour,[9] obtained under these ideal conditions with the
whirling-table, will be obtained in actual flight, at least with
plane wings.
The data in “Aerodynamics” were, then, insufficient to determine the
conditions of free flight, not alone because the apparatus compels
the planes to move in horizontal flight, but because other ideally
perfect conditions are obtained by surfaces rigidly attached to the
whirling-table so as to present an angle to the wind of advance
which is invariable during the course of the experiment, whereas
the surfaces employed in actual flight may evidently change this
angle and cause [p007] the aerodrome to move upward or downward,
and thus depart from horizontal flight so widely as to bring prompt
destruction.
Public-domain text, read in full here on John Shaqi.
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