Page:Aerial Flight - Volume 1 - Aerodynamics - Frederick Lanchester - 1906.djvu/279

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THE AEROFOIL.
§ 179

field of force symmetrical about the plane will also represent the upward momentum communicated to the air in partially arresting its downward motion during recess.

And the air outside the surfaces and will be receiving upward momentum the whole time it is in the field. Let the sum of this momentum be denoted by

Now, since the total residuary momentum must be zero (§§ 5 and 117) the downward momentum remaining in the air between the surfaces and is also equal to , and if be the downward momentum in the air when it quits the descending field we shall have:

But according to the main hypothesis we may represent by that is

It remains for us to assess the value of in terms of

Let us suppose that, in a manner analogous to the limitation of the sweep, the air external to the surfaces be represented by the limited region cut off by two further surfaces and then it is evident that the distance separating these surfaces will be greater the greater the lateral extension of the aerofoil.

Calling the fore and aft dimension of the aerofoil unity, so that its lateral dimension will let us assume that the distance between and is proportional to and let it be denoted by We have no direct means of testing the accuracy of this assumption; we can only say that it is a reasonable assumption, since the conditions that influence the depth of the layer of air acted upon obviously affect the extent of the disturbance of the fluid in other directions.

Then the upward momentum received by the air at the time of its crossing the plane is, from considerations of field symmetry, just half the total eventually imparted, that is but we

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