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
In the launching of Aerodrome No. 5, above described, it showed
no tendency to drop immediately upon leaving the launching ways,
but on the contrary its bow in every case rose almost immediately
until it was at an angle of about fifteen degrees or more. From
the photograph (Plate 35) it will be noticed that the wings of the
aerodrome are held down by the longitudinal strips, ‹A›, fastened to
cross-beams attached to the launching car. If, now, the launching
speed is too great and the aerodrome tries to rise immediately upon
being released, the front end, which passes from under the launching
car before the rear does, and is thus free to rise, will immediately
rise, while the rear cannot rise until it has passed entirely in
front of the car, which being a distance of several feet requires
an appreciable fraction of a second, during which time the bow of
the machine has been able to rise to quite a steep angle. This has
the effect of slowing down the aerodrome so that it does not get
quite the proper chance to start on its flight with a minimum head
resistance.
In view of the above facts, it was decided to decrease the speed of
the launching car slightly when using Aerodrome No. 5, so that this
matter could be thoroughly tested out.
[Illustration: PL. 35
AERODROME NO. 5 ON LAUNCHING-WAYS]
[p143]
JULY 11 TO JULY 14--AERODROME NO. 5
The very early morning preceding actual sunrise on July 11 was
undoubtedly as calm as it is possible to find; there was absolutely
no breeze stirring and the water in the river was as smooth as glass
as far as one could see. The anemometer cups were stationary, the
wind vane stood absolutely parallel to the launching apparatus and
everything promised a most successful experiment. After mounting
the aerodrome on the “overhead” launching apparatus the burner was
lighted, and while the steam pressure was still rising and the
propellers were revolving faster and faster all the time, there
was a snap and they ceased to turn. The fire, which was burning
fiercely, ran the pressure immediately to 150 pounds. An attempt
was at once made to start the propellers again by giving them an
initial turn by hand, it being thought possible that a sudden gush
of water had taken place and, accumulating in one end of the engine
cylinder, had blocked the engine. However, as the engine refused
to keep the propellers going after they were started, and as the
pressure was still rising very rapidly, the burner was shut off and
an investigation made. Upon removing the hull covering, it was found
that the connecting rod bearing had broken off short near the crank
pin of the engine, and that it would be necessary to take the part to
Washington in order to repair it, as there were no machine tools on
the house-boat.
Public-domain text, read in full here on John Shaqi.
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