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
AUGUST 3--AERODROME NO. 5
After the very satisfactory trial of Aerodrome No. 5 in the shop
two days previous, it was hoped, now that the weather had become
suitable, that a good flight with the superposed wings would be
obtained. The aerodrome, equipped with these wings, was accordingly
placed on the launching apparatus and the burners were lighted, but
they refused to work properly, a steam pressure of only 80 pounds
being obtained. After much delay the burners were finally got to
work properly, but the wind had increased in velocity to such an
extent that it was necessary to remove the aerodrome to the interior
of the house-boat. As the wind continued to increase in velocity it
was decided to make another trial of the aerodrome inside of the
house-boat. Upon doing this it was very soon found that there was a
small leak in the front turn of one of the coils of the boiler, and
the steam from this played directly against the burner, causing it
to work intermittently. A new coil was substituted, and after some
adjustment a very excellent run was obtained, the steam pressure
reaching 130 pounds and the propellers making 654 R. P. M.
In the afternoon the wind quieted down and the aerodrome, equipped
with superposed wings, was again placed on the launching apparatus.
The burners were lighted but again refused to work properly, the
vaporizing tip being stopped up with soot. This caused the burner to
“flood,” which sent a sheet of flame through the stack and burned the
rear right wing.
A new wing was substituted, the burner tip was cleaned out and
everything was again put in readiness for a flight. Upon lighting
the burners, 1 minute and 58 seconds were required to raise 120
pounds steam pressure. The underneath launching apparatus, with
the disappearing track, worked perfectly, the aerodrome dropping
slightly, but going straight ahead. It, however, continued to descend
for a distance of about 100 feet, the bow being elevated about
5 degrees. The bow then became horizontal, the aerodrome rising
slightly at the same time, but going only about 50 feet farther, when
it again started to descend slightly, and finally settled gently on
the water between 300 and 500 feet from the house-boat, with its bow
elevated about 3 degrees. There was a hiss as the hull touched the
water, showing that the fire was still burning and making it [p150]
improbable that the failure of the flight was due to lack of power.
The data on settings of wings, tail, etc., are given on Data Sheet
No. 11.
The speed of the launching car, one foot in front of the point at
which the aerodrome was released, was twenty feet a second, as shown
by the carbon record sheet carried by the launching car and moved in
front of a tuning fork which had been set in vibration.
Public-domain text, read in full here on John Shaqi.
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