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
On the following day a pair of the wings was inverted and a weight
of sand equal to the air pressure to which they were subjected in
flight, was distributed over their surfaces. Under the action of
this, the twisting of the wing was seen to increase from the root,
which was held with comparative rigidity, up to the tip, where in
spite of the cross-ribs it amounted to 45°. The resistance to torsion
lay chiefly in the front rib, which, in addition, could be bent
easily, allowing the surface to become distorted with great loss of
lifting power.
The experiments of 1894 had demonstrated the urgent necessity
for greater rigidity in the sustaining surfaces, which might, as
it seemed, be obtained either by increasing the strength of the
framing (which meant additional weight) or by resorting to some new
and untried construction, or by a proper system of guying. Guying
seemingly offered the most feasible solution of the problem; but
although the system of wire guying was thoroughly tried, the result
was very unsatisfactory, as the wings continued to twist and bag in a
way that was extremely discouraging.
1895
I accordingly had recourse in 1895 to the system of wooden guy-sticks
shown in Fig. ‹D›, Plate 16, which necessarily added greatly to
the weight of the sustaining surfaces. Each wing was separately
strengthened by means of a light rod of spruce, in cross-section
about the size of the main front rib, extending across the upper
surface of the wing, at a distance of about one-third the width of
the wing behind the front rib. It was tied to each of the cross-ribs
and to the outer bent portion of the front rib, and at its root was
fastened to the frame of the aerodrome.
This effectually prevented the bending of the front rib and the
consequent bagging of the cover, and to that extent marked a decided
advance in wing construction. But it was faulty, in that, not being
supplemented by wire guying, it offered little resistance to the
twisting of the wing about the main front rib, the rear tip of the
wing being free to turn up under pressure, as it had done on former
occasions. A similar guy-stick was stretched across the tail. To
guard against torsion, rods extending diagonally across the wings and
tail were used, which, with the aid of the guy-sticks just described,
prevented the surfaces from twisting greatly. In addition, a rod
joining the front ribs and stretching across from wing to wing tended
to maintain a fixed diedral angle. [p086]
Public-domain text, read in full here on John Shaqi.
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