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
Both the tests on the whirling-table and the actual results with the
models had shown that propellers which were true helices formed out
of wood were rather more efficient than those constructed by the use
of a hub in which were inserted wooden arms, forming a framing over
which cloth was tightly drawn. But the very great difference in the
cost of construction and the facility with which the latter type
could be repaired in case of damage—the wooden ones were practically
of no use if once they were much injured-—made it seem advisable to
construct all the propellers for the large aerodrome in the manner
just explained. Several pair of small propellers had been built on
this plan, some as early as 1895, and one very important advantage
had been found to be possessed by this type besides cheapness and
facility of repair. Wooden propellers of even so small a diameter as
one metre had been found to suffer a quite appreciable bending of the
blades, due to the thrust produced by them, even though the blades
had been made of considerable thickness. In planning a propeller 2.5
metres in diameter for the large aerodrome it was seen that in order
to make the blade sufficiently strong to withstand its own thrust it
would be necessary to make it inordinately thick, which, of course,
would mean a considerable increase in weight. In fact, it was seen
that the weight of the larger propellers would increase practically
as the cube of the diameter; which, for the 2.5-metre propeller,
would involve a weight of something over fifteen times the weight of
those one metre in diameter. The other type, which for convenience
we will call “canvas covered,” permitted the bending moment produced
on the blade by the thrust to be taken up by guy-wires running from
the corners of the blades to a central post projecting from the hub
of the propeller, and it was found that in this way a considerable
saving in weight could be effected. [p179]
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