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
With reference to the supporting and guiding surfaces of Aerodromes
Nos. 4, 5, and 6, Aerodrome No. 4, in its earliest condition
mentioned in the preceding chapter, was taken into the field, but
never brought to trial in the air. It is sufficient to say that in
the largest of the three sets of wings constructed, each wing was
17×51 inches, and therefore contained about six square feet, so that
with the tail (which was at this time a supporting surface), whose
area was one-half that of the two wings, the total supporting surface
was 18 square feet, or since the flying weight was 9.1 pounds, the
proportion of surface to weight was somewhat less than 2 square feet
to the pound. The wings were at this time ribless, it being expected
that the silk cover which was purposely left loose would take its
curve from the air filling it, which subsequent experience has
shown would have led to certain disaster if the aerodrome had been
launched. It may be added that there was a vertical rudder of what is
now seen to have been a wholly inadequate size. These remarks may be
applied with little modification to the attempted flight with No. 4
on May 25, except that the vertical rudder had been made larger, but
was still much too small.
1894
From the account of the field trials to be given in Chapter IX, it
will be seen that in numerous attempts at flight prior to October
6, 1894, the cause of failure can in every instance be traced to
imperfections more fundamental than those of the sustaining surfaces,
either the launching device or some other part failing to work
satisfactorily. I therefore commence a description of the sustaining
surfaces with those of Nos. 4 and 5 as used on that day.
The construction of the wings of No. 4 and No. 5, which were nearly
identical, is shown in Fig. ‹A› Plate 16. A rod of hickory, tapering
from 1/2 inch in diameter at the larger end to 1/4 inch at the
smaller, was steamed and bent, as shown in the drawing, to form the
main front rib of the wing. This was firmly clamped to the midrod,
and to the rib in turn were attached a number of cross-ribs of
hickory, slightly curved, the inner one of which was fastened to the
hull at its inner extremity, while the whole was covered with silk.
The length of each wing was 162 cm. (63.75 inches), and the width
54 cm. (21.25 inches). The tail was plane and equal in area to one
of the wings, so that the joint area of the wings and tail was 2.62
square metres (28.2 sq. ft.). [p082]
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