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
As soon as the workmen had had their breakfast, Aerodrome No. 5 was
again placed on the launching apparatus, equipped this time with
the superposed wings and Pénaud tail. Upon lighting the burners, it
was found that they did not work properly, a small piece of soot
having clogged up the tip of the vaporizing coil. While this trouble
with the burners was being remedied, the wind increased to such an
extent that it was found necessary to remove the aerodrome from the
launching apparatus to prevent its being injured by side gusts. As
it was Saturday and the wind showed no signs of quieting down, the
experiments were discontinued until the next week.
AUGUST 1--AERODROME NO. 5
After placing the aerodrome on the launching apparatus and getting
everything in readiness for a flight, upon lighting the burners a
sudden sheet of flame shot out of the smoke-stack and so seriously
charred three panels of each of the rear wings that they had to be
removed for repairs. The silk covering of the wings had been coated
with a special fire-proofing preparation, but the intensely hot
flame, of course, charred all the silk that it came in contact with.
By the time that the wings had been repaired, and the defect in the
burner which caused the accident had been remedied, a severe storm
had arisen, making it necessary to remove everything to the interior
of the boat. While waiting for the weather to become more suitable,
a test of the engine of Aerodrome No. 5 was made inside of the
house-boat. In this test a steam pressure of 140 pounds was obtained,
giving 650 R. P. M. of the round-end, 100-centimetre propellers,
which previous tests had shown to mean a thrust of 7480 grammes. As
the flying weight of the aerodrome was now 14,104 grammes, the thrust
obtained would correspond to a lift of 53 per cent of the flying
weight, which was maintained in this test for 90 seconds.
As the ‹CG› of Aerodrome No. 5 seemed to be a little too far forward
in the flight of July 28, it was decided to change it slightly, and
it was moved back 4 millimetres.
[Illustration: PL. 36
PATHS OF FLIGHT OF AERODROME NO. 5, JULY 29, 1899]
A trial run in the house-boat was also made on Aerodrome No. 6, while
waiting for the weather to become more suitable, but, unfortunately,
the result of this test was disastrous. The aerodrome had been placed
on trestles and [p149] held down to the floor by wires fastened to
the cross-frame. In the midst of the test one of the wires slipped,
allowing the aerodrome to push forward and thus permitting the
propellers to come in contact with the wires which held it to the
floor. Both propellers were entirely demolished and the cross-frame
was broken off short just at the right-hand engine. The disaster was
entirely due to the carelessness of one of the workmen in tightening
one of these wires, a further example of the extreme heedlessness of
workmen, even in the most important details, which concern the very
existence of the machine.
Public-domain text, read in full here on John Shaqi.
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