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
After several days of incessant rain and strong winds, which
prevented an experiment, the weather became brighter and the wind
quieted down and the afternoon of June 30 was almost ideal for an
experiment. At five o’clock Aerodrome No. 5, with “single-tier” wings
and Pénaud tail, was placed on the launching apparatus, a few minutes
later the burners were lighted, and just as the propellers started to
turn a racking noise was heard. Upon investigation it was found that
the circulating pump had broken. The break was a very small matter
and could have been repaired in an hour, but it was then too late to
repair the damage and get a flight before dark, so the aerodrome was
reluctantly dismounted and the men put to work repairing the broken
pump. [p142]
JULY 1 TO JULY 8
The great disadvantage of conducting the experiments at a point forty
miles from the city and the shops was felt at all times. Workmen,
even of the very best class, cannot be kept contentedly at work at a
point so far removed from their homes, even by bringing them to the
city on Saturday afternoon and carrying them back to the experimental
grounds the following Monday. Moreover, it is worse than useless to
try to get even as much as one-third the ordinary amount of work
done if there is the slightest excuse for tightening anchor ropes,
watching passing boats, or wasting time on any of the multitudinous
small variations from their usual routine of life.
On July 7, Aerodrome No. 5, equipped with “single-tier” wings and
Pénaud tail, was made ready for a flight in the afternoon. The
settings of the wings, tail, etc., are given on Data Sheet 6. Using
the “overhead” launching apparatus, the aerodrome was launched with a
steam pressure of 115 pounds. Immediately upon being launched its bow
rose to an angle of about fifteen degrees or more, and the aerodrome
came backward and downward and touched the water about three or four
feet from the house-boat.
It may be well to recall from what has been said in Part I, Chapter
IX, that Aerodrome No. 5 is the one with the very low thrust line,
and in 1896 had its “separator” several centimetres in front of its
center of gravity. When this aerodrome was overhauled just previous
to these experiments, the separator was moved back to the same
relative position as that in Aerodrome No. 6, so that the gradual
depletion of the water supply during flight would not cause it to
become light in front of the center of gravity.
Public-domain text, read in full here on John Shaqi.
Reviews
Reviews
No reviews yet
Be the first to share your thoughts on this work.
Elsewhere in the archive
Join the Discussion
Join the discussion
Sign in to leave a comment or review.
Sign InorCreate an account