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is needed for its support in the air。
Comparison With Aeroplanes。
If we compare the bird figures with those made possible
by the development of the aeroplane it will be
readily seen that man has made a wonderful advance in
imitating the results produced by nature。 Here are the
figures：
Supporting
Weight Surface Horse area
Machine in lbs。 in sq。 feet power per lb。
Santos…Dumont 。 。 350 110。00 30 0。314
Bleriot 。 。 。 。 。 700 150。00 25 0。214
Antoinette。 。 。 。 1；200 538。00 50 0。448
Curtiss 。 。 。 。 。 700 258。00 60 0。368
Wright。 。 。 。 。＇4＇1；100 538。00 25 0。489
Farman。 。 。 。 。 。 1；200 430。00 50 0。358
Voisin。 。 。 。 。 。 1；200 538。00 50 0。448
＇4＇ The Wrights' new machine weighs only 900 pounds。
While the average supporting surface is in favor of
the aeroplane； this is more than overbalanced by the
greater amount of horsepower required for the weight
lifted。 The average supporting surface in birds is about
three…quarters of a square foot per pound。 In the average
aeroplane it is about one…half square foot per pound。
On the other hand the average aeroplane has a lifting
capacity of 24 pounds per horsepower； while the buzzard；
for instance； lifts 5 pounds with 15…100 of a horsepower。
If the Wright machinewhich has a lifting power of 50
pounds per horsepowershould be alone considered the
showing would be much more favorable to the aeroplane；
but it would not be a fair comparison。
More Surface； Less Power。
Broadly speaking； the larger the supporting area the
less will be the power required。 Wright； by the use of
538 square feet of supporting surface； gets along with an
engine of 25 horsepower。 Curtiss； who uses only 258
square feet of surface； finds an engine of 50 horsepower
is needed。 Other things； such as frame； etc。； being equal；
it stands to reason that a reduction in the area of
supporting surface will correspondingly reduce the weight
of the machine。 Thus we have the Curtiss machine with
its 258 square feet of surface； weighing only 600 pounds
（without operator）； but requiring double the horsepower
of the Wright machine with 538 square feet of surface
and weighing 1；100 pounds。 This demonstrates in a
forceful way the proposition that the larger the surface
the less power will be needed。
But there is a limit； on account of its bulk and
awkwardness in handling； beyond which the surface area
cannot be enlarged。 Otherwise it might be possible to
equip and operate aeroplanes satisfactorily with engines
of 15 horsepower； or even less。
The Fuel Consumption Problem。
Fuel consumption is a prime factor in the production
of engine power。 The veriest mechanical tyro knows in
a general way that the more power is secured the more
fuel must be consumed； allowing that there is no difference
in the power…producing qualities of the material
used。 But few of us understand just what the ratio of
increase is； or how it is caused。 This proposition is one
of keen interest in connection with aviation。
Let us cite a problem which will illustrate the point
quoted： Allowing that it takes a given amount of gasolene
to propel a flying machine a given distance； half the
way with the wind； and half against it； the wind blowing
at one…half the speed of the machine； what will be
the increase in fuel consumption？
Increase of Thirty Per Cent。
On the face of it there would seem to be no call for
an increase as the resistance met when going against the
wind is apparently offset by the propulsive force of the
wind when the machine is travelling with it。 This； however；
is called faulty reasoning。 The increase in fuel
consumption； as figured by Mr。 F。 W。 Lanchester； of the
Royal Society of Arts； will be fully 30 per cent over
the amount required for a similar operation of the machine
in still air。 If the journey should be made at right
angles to the wind under the same conditions the increase
would be 15 per cent。
In other words Mr。 Lanchester maintains that the work
done by the motor in making headway against the wind
for a certain distance calls for more engine energy； and
consequently more fuel by 30 per cent； than is saved by
the helping force of the wind on the return journey。
CHAPTER XIV。
ABOUT WIND CURRENTS； ETC。
One of the first difficulties which the novice will
encounter is the uncertainty of the wind currents。 With a
low velocity the wind； some distance away from the
ground； is ordinarily steady。 As the velocity increases；
however； the wind generally becomes gusty and fitful
in its action。 This； it should be remembered； does not
refer to the velocity of the machine； but to that of the
air itself。
In this connection Mr。 Arthur T。 Atherholt； president
of the Aero Club of Pennsylvania； in addressing the
Boston Society of Scientific Research； said：
〃Probably the whirlpools of Niagara contain no more
erratic currents than the strata of air which is now immediately
above us； a fact hard to realize on account
of its invisibility。〃
Changes In Wind Currents。
While Mr。 Atherholt's experience has been mainly
with balloons it is all the more valuable on this account；
as the balloons were at the mercy of the wind and their
varying directions afforded an indisputable guide as to
the changing course of the air currents。 In speaking of
this he said：
〃In the many trips taken； varying in distance traversed
from twenty…five to 900 miles； it was never possible
except in one instance to maintain a straight course。
These uncertain currents were most noticeable in the
Gordon…Bennett race from St。 Louis in 1907。 Of the
nine aerostats competing in that event； eight covered a
more or less direct course due east and southeast； whereas
the writer； with Major Henry B。 Hersey； first started
northwest； then north； northeast； east； east by south； and
when over the center of Lake Erie were again blown
northwest notwithstanding that more favorable winds
were sought for at altitudes varying from 100 to 3；000
meters； necessitating a finish in Canada nearly northeast
of the starting point。
〃These nine balloons； making landings extending from
Lake Ontario； Canada； to Virginia； all started from one
point within the same hour。
〃The single exception to these roving currents occurred
on October 21st； of last year （1909） when； starting
from Philadelphia； the wind shifted more than eight
degrees； the greatest variation being at the lowest altitudes；
yet at no time was a height of over a mile reached。
〃Throughout the entire day the sky was overcast； with
a thermometer varying from fifty…seven degrees at 300
feet to forty…four degrees； Fahrenheit at 5；000 feet； at
which altitude