The problem has also been attacked from an entirely different angle and a theory was propounded by W. Froude in which the action of each elementary portion of the blade surface is sepa rately estimated from the forces on planes moved through water at various speeds and at different angles of obliquity (see Trans. I.N.A. 1878). The investigation is of importarice though it does not completely represent the actual conditions; for the deduc tions from a small element moving through undisturbed water are applied to the whole blade ; the disturbance of the water when a blade reaches it and the consequent effects of each element on adjoining elements and of one blade on another are not taken into account. The momentum theory of R. E. Froude has been strikingly confirmed by some exhaustive experiments in a wind channel; and it is found that when the velocity deduced from this theory combined with certain interference factors is applied to the blade element theory of W. Froude in the light of modern experiment data, good agreement is obtained with actual practi cal results in the case of narrow bladed screws such as air pro pellers.
In recent years the general application of the circulation theory to hydrodynamical problems has resulted in the conception of the vortex theory of the screw propeller. This theory when more fully developed promises not only to clarify the physical nature of propeller action but to assist the quantitative estimating of propeller performance. The large wide blades used in marine propellers and the confused nature of the water flow at the stern of a ship make the application of theory to all marine screw pro peller problems extremely complicated.
a very complete range and the results can be used for most prac tical problems. (See Trans. I.N.A. 1908.) The thrust horse power is given by Froude in the following formula :— where H is the thrust horsepower, V speed of advance in knots and D the diameter in feet ; p is the effective pitch ratio calcu lated from the revolutions for zero thrust. For full sized screws Froude considers this is 1.02 times the face pitch ratio ; for mod ern screws it is probable that the ratio should exceed 1.02. The "blade factor" B depends only on the type and number of blades; its value for various "disc area ratios," i.e., ratio of total blade area (assuming the blade to extend to the centre of shaft) to the area of a circle of diameter D is given in the following table :— Reference should be made to the paper for curves of efficiency obtained.
The influence of the screw also extends sufficiently far forward to cause a diminution of pressure on the after part of the ship, thereby causing an increase in resistance. The thrust T, exerted by the screw working behind the ship must be sufficient to bal ance the tow rope resistance R. This increase of resistance as well as this diminution of pressure is conveniently expressed as a fraction t of the thrust exerted by the screw, whence it follows that TO —1)=R. The power exerted by the propeller or the thrust horsepower is proportional to T X (V—V'); the effective horsepower is R x V and the ratio of these two, is termed the hull efficiency. The hull efficiency value does not differ greatly from unity with different positions of the screw. An account of an interesting series of experiments to determine the values of w and t is given by W. J. Luke, Trans. I.N.A. 1910.