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 struts referred to above were three in number, two being placed
near the rear and one at the center of the front of the car. The use
of three points of support had the advantage of furnishing a rather
rigid foundation against which the frame could be tightly drawn by
means of the clutch-hook without risk of straining it. In designing
the “underneath” launching apparatus, which was very thoroughly
tested in the experiments with the models in the summer of 1899, the
plan of having three struts with the aerodrome drawn tightly against
them by means of a central clutch-hook was continued with most
satisfactory results.
When the position of the struts on this launching apparatus had been
changed so as to permit it to be used for the quarter-size model,
it was found, in making shop tests of the engine with the aerodrome
mounted on the launching car, that, owing to the greater vibration
produced by the gasoline engine, the three points of suspension
did not hold the model in a sufficiently rigid manner. It became
necessary, therefore, to use four struts, the two rear ones being
left as before, and the single one in front being replaced by two
interconnected ones arranged similarly to those in the rear. After
making this change no difficulty was found in holding the aerodrome
rigidly against the struts, and this modification was therefore
immediately introduced in the designs for the large launching car
which was already under construction.
[Illustration: PL. 39
METHOD OF ATTACHING GUY-WIRES TO GUY-POSTS TO RELIEVE TORSIONAL
STRAIN]
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