the rotary type, in lightness and ease of fitting into the nose of a
fuselage. The majority of machines were tractors (propeller in front)
although a preference, which died down subsequently, was still shown for
the monoplane over the biplane. This year also saw a great increase
in the number of seaplanes, although the 'flying boat' type had only
appeared at intervals and the vast majority were of the ordinary
aeroplane type fitted with floats in place of the land undercarriage;
which type was at that time commonly called 'hydro-aeroplane.' The usual
horse power was 50--that of the smallest Gnome engine--although engines
of 100 to 140 horse-power were also fitted occasionally. The average
weight per horse-power varied from 18 to 25 lbs., while the wing-loading
was usually in the neighbourhood of 5 to 6 lbs. per square foot. The
average speed ranged from 65-75 miles per hour.
III. PROGRESS ON STANDARDISED LINES
In the last section an attempt has been made to show how, during what
was from the design standpoint perhaps the most critical period, order
gradually became evident out of chaos, ill-considered ideas dropped out
through failure to make good, and, though there was still plenty of room
for improvement in details, the bulk of the aeroplanes showed a general
similarity in form and conception. There was still a great deal to be
learnt in finding the best form of wing section, and performances were
still low; but it had become definitely possible to say that flying had
emerged from the chrysalis stage and had become a science. The period
which now began was one of scientific development and improvement--in
performance, manoeuvrability, and general airworthiness and stability.
Public-domain text, read in full here on John Shaqi.
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