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
It was also found after the experiment that one of the workmen, in
assembling the machine on the launching car, had secretly increased
the stiffness of the spring which controls the elasticity of the
Pénaud tail. The effect of this increase in the stiffness of the
Pénaud tail might at first thought appear to be similar to that
of moving the center of pressure forward. Upon a closer analysis,
however, it will be seen that the effect is very much greater, as
excessive stiffness of the Pénaud tail not only causes the aerodrome
to elevate its bow, [p140] but requires the overcoming of a strong
downward force at the rear, even more serious than would be caused by
placing an extra load at the rear of the machine without regard to
its effect on the balancing. In experiments of this kind, however,
the workmen get certain ideas of their own as to how the work should
be conducted, and it is almost impossible in assembling the aerodrome
to prevent them from making adjustments which are quite different
from those which they have been directed to make, and which have been
definitely planned with a view to determining the effect of slight
changes which it is desired shall not be masked by changes of any
kind in other details.
JUNE 23--AERODROME NO. 6
The wind, which had been blowing half a gale all day, gradually
quieted down towards sunset and at five o’clock was very light,
blowing only two miles an hour from the east-southeast. As one of
the rear superposed wings had been injured on the previous day in
carrying the aerodrome into the house-boat after its short and
erratic flight, it was decided to use the “single-tier” wings in
this experiment, and also to continue using the “overhead” launching
apparatus for a few more flights. Everything being in readiness,
the burners were lighted and 70 seconds were consumed in raising a
steam pressure of 120 pounds, at which pressure the aerodrome was
launched. It started straight ahead, dropping not more than a foot,
and flying on an absolutely even keel for about 800 feet, when it
suddenly turned to the left and made a short half circle of about
100 feet diameter, heading for a point about 150 feet east of the
house-boat. When it was about 200 feet from the shore, a sudden gust
of wind caught under the Pénaud tail, raising the rear portion of the
aerodrome and causing the bow to point down at an angle of about 30
degrees. The aerodrome kept this angle and struck the shallow water
only about 20 feet from the shore. The aerodrome was comparatively
uninjured, and another flight would have been made immediately
but for the fact that by the time the aerodrome had been properly
inspected it was quite late, and entirely too dark, and there would
have been danger of losing it in the adjacent marshes, which are
difficult to traverse even under the best conditions of tide and
light. The path of this flight is shown by the dotted line in Plate
34.
JUNE 27--AERODROME NO. 5
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