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
In view of the disasters from trials in the field, due to inability
to obtain automatic equilibrium in flight and to the flexure of the
large wings rather than to defects of the engines, the conditions at
this time, after three years of failure, seemed so nearly hopeless,
that without abandoning the work on these steam aerodromes, I again
had recourse to the early plan of constructing smaller models driven
by India rubber, in which the small wings employed could be made
of the requisite stiffness. Instead of employing twisted rubber,
however, the defects of which had been amply proved in previous
trials, these new constructions were meant to employ rubber directly
stretched and pulling. In this condition the rubber exercises nearly
six times the power in proportion to weight that it does when
twisted, but on the other hand it requires a very strong frame and
subordinate parts.
I spent an inordinate amount of time and labor during this year in
attempting to employ this latter form of construction and finally got
a few useful results from it, but none in proportion to the labor
expended.
During March, Aerodrome No. 5, the frame of which had proved on
test to be radically weak, was completely refinished except for
the wings. The propellers had hitherto been made of wood, but in
May, I commenced a new construction of steel, wood and cloth, on a
plan giving a figure which, though not rigorously helicoidal, was
practically near enough to the theoretical form and was also both
lighter and more elastic than the wooden construction.
On May 8 and June 7 Aerodrome No. 5 was again tried at Quantico, and
although the tests were unsuccessful, in that the aerodrome failed
to fly, partly because of the fact that so much time was spent in
raising steam that practically the entire supply of fuel and water
was exhausted before the aerodrome was actually launched, yet it had
come so much nearer flying than any machine had previously done,
that it was felt that if either the power could be increased or the
weight decreased even a slight amount, the aerodrome would probably
fly. In view of the great care that had been exercised in keeping
down the weight, it seemed almost hopeless to attempt to reduce it,
and it also seemed equally hopeless to attempt to get more power
without increasing the weight. However, something had to be done to
increase the ratio of power to weight, and as it was seen that this
would involve extensive changes in No. 5, it was decided to entirely
rebuild No. 4 with this idea in view, though it was evident that it
involved a plan of construction even lighter than the dangerously
light plan on which No. 4 had already been constructed.
Public-domain text, read in full here on John Shaqi.
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