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
At 9.45 a. m., the wings having been dried, No. 5 was again tried.
The float was moved back to its normal position at the base of the
bowsprit, and the guys, by which the outer ends of the tail had been
depressed in the previous trial, were so adjusted that the tail was
flat. The machine was, therefore, in the condition of theoretical
equilibrium for rapid motion with a plane wing. All the other
conditions were precisely as in the previous trial, except that
the round-end 100-centimetre propellers were substituted for the
95-centimetre ones which had been broken, and a new paper-covered
tail was used. The mechanic in charge was directed to let the steam
reach its highest pressure consistent with a flight of one-half a
minute, before launching the machine, but he seemed to have lost all
sense of the length of time the fuel and water would last, as he let
the engines run until almost the whole charge was exhausted before
launching it. The aerodrome went off almost horizontally, then turned
up into the wind and rose to an angle of about twenty degrees; then
(while moving forward) slowly sank as though the engine power had
given out, as in fact it doubtless had. The actual distance travelled
was 123 feet and the length of time 7.2 seconds. While the exhaustion
of the fuel and water prior to launching the machine had prevented
what apparently would otherwise have been an [p104] exceedingly good
flight, yet the fact that the aerodrome rose immediately after being
launched, and continued to do so until the power gave out, was in
itself very encouraging.
At 1.40 p. m. No. 5 was again ready for trial (the third one for
the day), and this time Mr. Langley and Dr. Bell witnessed it from
a greater distance in hopes of being able more clearly to study its
behavior when actually in the air.
The previous trial having missed success through the fuel and water
having been consumed before the machine was launched, special
instructions were given to avoid the recurrence of this mistake. But
the machine was held for probably two minutes after the burners were
lighted, with very much the same result as before. The conditions of
the aerodrome were the same as in the previous trial, except that the
tail was a little flatter, so as to tend to make the head slightly
lower in flight. It was launched at an angle of about thirty degrees
with the very gentle wind that was blowing, and, apparently under
the direction of the rudder, turned into the wind, the midrod rising
to an angle of about twenty degrees and (as noted in Mr. Langley’s
record book) “The whole machine absolutely rising during five or
six seconds--a fine spectacle! Then the power visibly gave out, the
propellers revolving slower. It settled forward and lost nearly all
of its forward motion at the end of about seven seconds, but did not
finally touch the water until ten and a quarter seconds.”
Public-domain text, read in full here on John Shaqi.
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