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
very materially to the general strength of the frame, no important
changes were made in No. 5 prior to its remarkable flight of May 6,
1896.
[Illustration: PL. 14
AERODROME NO. 5, DECEMBER 3, 1895. PLAN VIEW. RUDDER REMOVED]
[Illustration: PL. 15
AERODROME NO. 5, DECEMBER 3, 1895. SIDE VIEW]
While these changes were being made in No. 5, similar ones were
also being carried out in New No. 4, and the addition of the rear
wings to No. 4, together with other slight changes, made it such a
distinctively different machine from what it had been, that it was
now designated as No. 6. After making extensive [p079] repairs
to the extremely light frame of No. 6 (formerly New No. 4) it was
thought to be in suitable condition for flight and was accordingly
boxed preparatory to sending it to Quantico.
The year, therefore, closed with No. 6 apparently in condition for
test, but it was decided not to take it to Quantico until No. 5,
which was still undergoing repairs, could also be got ready.
1896
A few days after the beginning of the new year, while the repairs on
No. 5 were being completed, it was decided that the frame of No. 6
which had been boxed ready to be carried into the field for trial,
was so weak that before putting it to an actual test in flight it
would be best to make some tests on the strength of its frame. While
testing the frame for torsional strength, it broke under the moderate
test of a weight of 500 grammes placed at the tips of the wings, the
angle of deflection just prior to its breaking being 35°, while the
frame of Old No. 4 in March, 1895, had shown a deflection of only
10.5° under a similar test. This breaking of the frame showed very
plainly that the worst fears in regard to it had been realized and
that by some means or other the frame must be strengthened. This was
finally accomplished by making the midrod continuous through the
smoke-stack as had already been done in No. 5, and at the same time
an additional improvement was made in the means of attaching the
Pénaud tail, whereby it was lowered in order to give it a greater
clearance in passing under the launching car in actual test. Later
the boilers proved defective and new ones were substituted, but
except for some minute details no further changes were made in
Aerodrome No. 6 prior to its test in May.
On May 6, No. 6 was unsuccessfully tried at Quantico just prior to
the very successful test of No. 5. In this test no serious damage
was done to the frame, but before going to Europe in the summer, Mr.
Langley ordered that both aerodromes be completely overhauled and put
in condition for further experiments in the fall. In this remodelling
practically no changes were introduced in the frame of either No. 5
or No. 6, but the engines of No. 6 were refitted and a new boiler was
substituted, which, with slight improvements in the burner, resulted
in a somewhat increased power in the engines.
Public-domain text, read in full here on John Shaqi.
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