| ANALYSIS OF PROPELLER FORCES | | Print | |
| Written by sivasankar |
| Tuesday, 17 November 2009 17:47 |
Mathematical Analysis Of Propeller ForcesWHAT A PROPELLER DOES?
ASSUMPTION: * In this theory, the propeller is considered as an actuator disc. * An actuator disc is a disc which performs water movement. The disc imparts axial acceleration to the water.
let, A - Area of actuator disc, Po- Ambient pressure ( pressure of water initially and finally ), dp- Increase in pressure at the tip of the disc, va- Speed of advance of the screw, ava- Initial velocity of water, bva-Final velocity of water, Now, velocity of water relative to disc is = va + ava = va(1+a) where a- axial inflow factor Mass of water acted on per unit time is M= = (Density X volume of water)/ time = ρ X area X (length / time) = ρ X area X velocity = ρ A va (1+a) change of momentum = mass X velocity = ρ A va (1+a) X bva
Equating this change of momentum to the thrust, T = ρ A va2 ( 1 + a ) b We know that the work done by the thrust on water is given by the product of the thrust and the velocity, = T X ava = ρ A va2 ( 1 + a )b X ava = ρ A va3( 1 + a ) X ab We know that the work done is equal to kinetic energy in water column ρ A va3( 1 + a ) X ab = work done kinetic energy in water column k.e. = (1/2) X m X v2 = (ρ A va (1+a)(bva)2 ) / 2 kinetic energy = work done ρ A va3( 1 + a ) X ab = ρ A va3( 1 + a ) b2 / 2 a = b/2
The useful work done by the disc is equal to the product of thrust and the forward velocity Useful work done = ρ A va2 ( 1 + a )b X va = ρ A va3 ( 1 + a )b The total work done is the sum of the above two work done: = ρ A va3 ( 1 + a )b + ρ A va3( 1 + a ) X ab = ρ A va3 (1+a) [ ab + b ]
η = (ρ A va3 ( 1 + a )b) /( ρ A va3 (1+a) [ ab + b ] ) η = 1/(1+a)
Till now we have considered only the axial velocity imparted to the water, but in case of a real propeller, because of the rotation of the propeller, the water will also have rotational velocity imparted to it by the propeller, and hence it has to be considered. Therefore the overall efficiency becomes, overall efficiency η = ( 1 - a' )/( 1 + a) where, a' - Rotational inflow factor, This means that, because of the rotational velocity the efficiency is further reduced. LIMITATIONS OF THIS THEORY:
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