FREE BOOKS

Author's List




PREV.   NEXT  
|<   94   95   96   97   98   99   100   101   102   103   104   105   106   107   108   109   110   111   112   113   114   115   116   117   118  
119   120   121   122   123   124   125   126   127   128   129   130   131   132   133   >>  
tations imposed on the motion of an aeroplane by wind velocity, Mr. Lanchester gave the diagrams shown in Figs. 1 to 4. The circle in each case was, he said, described with a radius equal to the speed of the aeroplane in still air, from a center placed "down-wind" from the aeroplane by an amount equal to the velocity of the wind. Fig. 1 therefore represented the case in which the air was still, and in this case the aeroplane represented by _A_ had perfect liberty of movement in any direction In Fig. 2 the velocity of the wind was half that of the aeroplane, and the latter could still navigate in any direction, but its speed against the wind was only one-third of its speed with the wind. In Fig. 3 the velocity of the wind was equal to that of the aeroplane, and then motion against the wind was impossible; but it could move to any point of the circle, but not to any point lying to the left of the tangent _A_ _B_. Finally, when the wind had a greater speed than the aeroplane, as in Fig. 4, the machine could move only in directions limited by the tangents _A_ _C_ and _A_ _D_. Matter of Fuel Consumption. Taking the case in which the wind had a speed equal to half that of the aeroplane, Mr. Lanchester said that for a given journey out and home, down wind and back, the aeroplane would require 30 per cent more fuel than if the trip were made in still air; while if the journey was made at right angles to the direction of the wind the fuel needed would be 15 per cent more than in a calm. This 30 per cent extra was quite a heavy enough addition to the fuel; and to secure even this figure it was necessary that the aeroplane should have a speed of twice that of the maximum wind in which it was desired to operate the machine. Again, as stated in the last lecture, to insure the automatic stability of the machine it was necessary that the aeroplane speed should be largely in excess of that of the gusts of wind liable to be encountered. Eccentricities of the Wind. There was, Mr. Lanchester said, a loose connection between the average velocity of the wind and the maximum speed of the gusts. When the average speed of the wind was 40 miles per hour, that of the gusts might be equal or more. At one moment there might be a calm or the direction of the wind even reversed, followed, the next moment, by a violent gust. About the same minimum speed was desirable for security against gusts as was demanded by other considerations. Si
PREV.   NEXT  
|<   94   95   96   97   98   99   100   101   102   103   104   105   106   107   108   109   110   111   112   113   114   115   116   117   118  
119   120   121   122   123   124   125   126   127   128   129   130   131   132   133   >>  



Top keywords:
aeroplane
 
velocity
 
direction
 
machine
 

Lanchester

 

motion

 

circle

 

average

 

journey

 

represented


moment

 

maximum

 

operate

 

desired

 

stated

 

demanded

 

addition

 
secure
 
figure
 

desirable


security

 

lecture

 
Eccentricities
 

reversed

 

violent

 

considerations

 
excess
 

liable

 

minimum

 
largely

automatic

 
stability
 

encountered

 

connection

 
insure
 

tangents

 

movement

 

liberty

 

perfect

 

amount


navigate

 
impossible
 
center
 

diagrams

 

imposed

 

tations

 

radius

 

require

 

needed

 
angles