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
Before proceeding with the construction of any more complete wings,
an extended series of experiments was made in order to secure ribs
of proper lightness and strength. Various forms of metal tubes were
tested; but, although aluminum seemed at one time to promise good
results, it was found that hollow ribs could be constructed of spruce
which were much stronger than aluminum tubes of the same weight. In
order to determine more accurately what mode of construction would
give the greatest stiffness and strength for a minimum weight, it was
decided to make up some test pieces of different forms before making
up complete ribs. For convenience in construction, these test pieces
were made straight and shorter than the large cross-ribs. Each piece
was tested by fastening it in the testing clamp with 1 metre of its
length projecting horizontally, and attaching at its end a weight of
1 kilogramme. The deflection from the horizontal gave an index of the
stiffness of the piece under examination.
The first test piece was a hollow square, 17 mm. length of side on
the exterior, and 11 mm. length of side on the interior, the walls
thus being 3 mm. thick. This weighed 73 grammes per metre and had
small internal stiffening pieces, like the partitions in bamboo,
glued into it 4 inches apart. A weight of 1 kilogramme at the
distance of 1 metre gave a deflection of 56 mm. The second test piece
was a duplicate of the first one, except that it had no internal
stiffening pieces, and the weight per metre was made the same, 73
grammes, as formerly, by leaving the walls a fraction thicker. The
deflection in this case was, as would be expected, exactly the same
as in the first one. The first test piece, however, was superior to
the second one in that it was stiffer against being crushed in by
accident. The third test piece was a hollow cylinder, 22 mm. outside
diameter and 17 mm. inside diameter, the walls thus being 2.5 mm.
thick. The weight per metre was 91 grammes, and the deflection was
46 mm. The fourth test was made by taking two of the original solid
cross-ribs, 12 mm. in diameter, and fastening them in the clamp side
by side, with a length of 1 metre projecting. The weight per metre
for the two ribs was 105 grammes, and the deflection produced on the
two by 1 kilogramme at 1 metre distance was 115 mm. The fifth test
piece was an I-beam of spruce, having a depth of 25 mm., with the
flanges 12.5 mm. wide and the web 3 mm. thick. The weight per metre
was 65 grammes, and the deflection was 26 mm. All of these test
pieces were made of carefully selected straight-grained spruce.
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