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
The perfected launching apparatus which had been used for the
steam-driven models Nos. 5 and 6 (described in Part I, Chapter X) had
proved most satisfactory and reliable, but when the designs were made
for a launching apparatus for the large machine it was found that
an exact duplication of the plan of the small one involved serious
difficulties in connection with the construction of the house-boat,
owing to the very considerable weight and size of the turn-table
necessary to permit the aerodrome to be launched in any desired
direction, regardless of the direction in which the houseboat might
be pointing under the influence of the wind and tide. A new design
was accordingly made for a launching apparatus in which the launching
car was to run on a track mounted directly on the turn-table, the
launching car supporting the aerodrome from underneath, instead of
being mounted in an inverted position on an overhead track with the
aerodrome depending from it.
From the previous description of the launching apparatus, it will be
recalled that, in order to provide that the aerodrome should drop
slightly at the moment of its release from the car, and thereby avoid
all danger of entanglement, the speed of the launching car at the
point at which the aerodrome was released was purposely made ‹less›
than the “soaring speed” of the aerodrome. Having this feature in
mind, when designing the “underneath” launching apparatus, it was
recognized that the danger of the aerodrome becoming entangled with
this form of apparatus could be avoided by making the launching
speed ‹greater› than the velocity which it would be necessary for
the aerodrome to have in order to soar, ‹provided the balancing was
correct and the aerodrome did soar›. Nevertheless, it was deemed
unwise to put too much dependence on the empirical calculations from
which the balancing of the large aerodrome would necessarily be
determined, and, therefore, some means seemed necessary for causing
the launching car to drop out of the way immediately upon releasing
the aerodrome. In the new design, more completely described below,
in Chapter IV, this was accomplished by so arranging a portion of
the front end of the track that, at the moment the launching car
released the aerodrome, it dropped like a disappearing gun carriage,
leaving the aerodrome free in the air with no possibility of becoming
entangled, provided the aerodrome itself did not drop more rapidly
than an angle of 15 degrees.
A small working model of this launching apparatus, one-eighth the
linear dimensions of that which would be necessary for the large
aerodrome, was first designed and constructed in the shop, the small
one-eighth-size model of the large aerodrome being launched from it
into a sheet stretched in front of it to act as a buffer. When it was
found to work very satisfactorily, a large one, twice this size, was
immediately built for use with the steam-driven models Nos. 5 and 6.
[p135]
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