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
Number of rib. Deflection.
Inches.
1 (Heavy end rib) 5.5
2 9.5
3 11.75
4 12.25
5 12.5
6 12.75
7 12.9
8 13.0
9 12.0
10 (Heavy end rib) 9.75
The weight of sand put on the wing in this test was 1.5 times as
great as the pressure which at this time it was expected would be
imposed upon it in flight, and was in fact 1.2 times as great as the
normal pressure when supporting the aerodrome as finally constructed.
Even under this weight the greatest deflection noted in terms of the
total length of the rib was less than 0.10, showing that the elastic
limit of the rib was far from being reached. [p204]
As this test seemed to indicate that the wings constructed in
this manner were certainly strong and rigid enough for use on the
aerodrome, and that immediate further improvement could hardly be
made, three similar wings were at once constructed to complete the
set. Somewhat later two additional wings were provided, so that when
the large aerodrome was taken to Widewater on the Potomac in 1903 one
and a half complete sets of wings were on hand, which seemed to be
ample to provide for any emergencies that might arise.
Each of these wings had, as is clearly shown in the drawings,
Plates 53 and 54, two main ribs, which formed the main strength
of the framework and gave the wing longitudinal rigidity. To the
main front rib were attached the cross-ribs and the pieces for the
curved extension later described. The mid-rib extended across the
cross-ribs, parallel to and about 5 feet behind the front rib, this
being approximately the line in which lay the center of pressure of
the wing. It was upon this rib, therefore, that the greatest strain
would fall.
The mid-rib, Plate 66, Fig. 2, was 731.5 cm. (24 ft.) long, having at
the butt an outer diameter of 38 mm. (1.5 in.) and an inner diameter
of 25 mm. (1 in.), the walls being, therefore, approximately 6.5 mm.
(0.25 in.) thick. From the butt to the middle point the section was
uniform, but from this point it had a taper of one-twenty-fourth of
an inch to the foot, so that at the tip it had an outer diameter of
25 mm. (1 in.), the thickness of the wall being unchanged. At the
butt end a wooden block 8 inches long was glued inside the rib, and
at uniform distances of 75 mm. (30 in.) 10 smaller blocks were glued
in where the cross-ribs were attached. The main front rib was of the
same form and size, except that it was some 2 inches shorter and had
no blocks, except the long one at the butt, glued in it.
Public-domain text, read in full here on John Shaqi.
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