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Momentum Equation and its Applications Moving fluid exerting force The lift force on an aircraft is exerted by the air moving over the wing. A jet of water from a hose exerts a force on whatever it hits. In fluid mechanics the analysis of motion is performed the same way as in solid mechanics by use of Newton's laws of motion. Properties of fluids considered when in motion F ma Used to analyze solid mechanics to relate applied force to acceleration In fluid mechanics not clear mass of moving fluid to use hence the use momentum equation. Statement of Newton's Second Law relates the sum of the forces acting on an element of fluid to its acceleration or rate of change of momentum. The Rate of change of momentum of a body is equal to the resultant force acting on the body, and takes place in the direction of the force Consider the streamtube: Assume flow to be steady and non-uniform 1 A1 u1 1 2 A2 u2 2 u1t In time δt a volume of the fluid moves from the inlet a distance uδt, Volume entering the stream tube in time δt Area distance A1u1t Mass entering stream tube in time δt volume density 1 A1u1t Momentum of fluid entering stream tube in time δt mass velocity 1 A1u1t u1 Similarly, at the exit, the momentum leaving the steam tube is 2 A2u2t u2 Calculate force on the fluid using Newton's 2nd Law Force = rate of change of momentum ( 2 A2 u2t u2 1 A1u1t u1 ) F t From continuity Q A1u1 A2 u2 Assume fluid of constant density 1 2 Hence F Q (u2 u1 ) or F M (u2 u1 ) Force acts in direction of flow of the fluid. Analysis assumed inlet and outlet velocities were in the same direction - one dimensional system. Consider two dimensional u2 2 1 u1 • At inlet the velocity vector, u1, makes an angle, θ1, with the x-axis. • At the outlet velocity, u2 makes an angle θ2. Resolve forces in the directions of the co-ordinate axes. The force in the x-direction Fx = Rate of change of momentum in x-direction = Rate of change of mass change in velocity in x-direction M (u2 cos 2 u1 cos1 ) M ( u2 x u1 x ) Q(u2 cos 2 u1 cos1 ) Q( u2 x u1 x ) The force in the y-direction Fy = Rate of change of momentum in y-direction = Rate of change of mass change in velocity in y-direction M (u2 sin 2 u1 sin1 ) M ( u2 y u1 y ) Q(u2 sin 2 u1 sin1 ) Q( u2 y u1 y ) The resultant force on the fluid Fresultant F F 2 x 2 y And the angle which this force acts at is given by tan ( 1 Fy Fx ) For three-dimensional (x, y, z) system an extra force in the z-direction must be calculated. This is considered in exactly the same way. Generally the total force on fluid = rate of change of momentum through the control volume F Q( uout uin ) This force is made up of three components: FR Force exerted on the fluid by any solid body touching the control volume FB Force exerted on the fluid body (e.g. gravity) FP Force exerted on the fluid by fluid pressure outside the control volume Total force, FT, given as the sum of these forces FT FR FB FP Force exerted by the fluid on the solid body touching the control volume is equal and opposite to FR So the reaction force, R, is given by R FR Application of the Momentum Equation Force due to fluid flow round a pipe bend Force on a nozzle at the outlet of a pipe. Impact of a jet on a plane surface. The force due to fluid flow round a pipe bend Consider a pipe bend with a constant cross section Lying in the horizontal plane Turning through an angle of θ°. Step in Analysis: 1. Draw a control volume 2. Decide on co-ordinate axis system 3. Calculate the total force 4. Calculate the pressure force 5. Calculate the body force 6. Calculate the resultant force 7. Find force on the fluid Control volume • The control volume is drawn with faces at the inlet and outlet of the bend and encompassing the pipe walls. Co-ordinate axis system Co-ordinate axis chosen such that one axis is pointing in the direction of the inlet velocity. Calculate the total force In the x-direction: F Tx Q( u2 x u1 x ) u1 x u1 In the y-direction: F Ty Q( u2 y u1 y ) u1 y u1 sin 0 0 u2 x u2 cos u2 y u2 sin F Tx Q(u2 cos u1 ) F Ty Qu2 sin Calculate the pressure force Fp Pressure force at 1 – pressure at 2 F px p1 A1 cos 0 p2 A2 cos p1 A1 p2 A2 cos F py p1 A1 sin 0 p2 A2 sin p2 A2 sin Calculate the body force There are no body forces in the x or y directions. The only body force is that exerted by gravity a direction we do not need to consider. Calculate the resultant force FT x FRx FB x FPx FT y FR y FB y FP y FR x FTx F p x FB x Q( u2 cos u1 ) ( p1 A1 p1 A1 cos ) 0 FR y FT y F p y FB y Qu2 sin ( p2 A2 sin ) 0 Resultant force on fluid is given as Direction of application Force on bend is the same in magnitude as force on fluid, but in opposite direction Example • A 45o reducing bend is connected in a pipe line in on a horizontal floor. The diameters at the inlet and outlet of the bend are 600 and 300 mm respectively. Find the force exerted by water on the bend if the intensity of pressure at the inlet to bend is 8.829 N/cm2 and rate of flow of water is 600 lit/sec. Force on a pipe nozzle Step in Analysis: 1. Draw a control volume 2. Decide on co-ordinate axis system 3. Calculate the total force 4. Calculate the pressure force 5. Calculate the body force 6. Calculate the resultant force 7. Find the force to resist Control volume and Co-ordinate axis 1 2 A1 A2 u2 u1 1 One dimensional system 2 Calculate the total force FT FTx Q( u2 u1 ) Continuity Q A1u1 A2 u2 1 1 FTx Q A2 A1 2 Calculate the body force The only body force is the weight due to gravity in the y-direction - but we need not consider this as the only forces we are considering are in the x-direction. Calculate the pressure force Apply Bernoulli equation to calculate the pressure 2 1 2 2 p1 u p2 u z1 z2 h f g 2 g g 2 g Frictional losses neglected, hf = 0 Nozzle is horizontal, z1 = z2 Q 1 1 p1 2 2 2 A2 A1 Pressure outside is atmospheric, p2 = 0 2 Calculate the resultant force FTx FRx F p x FB x FRx FTx F p x 0 FRx 1 1 Q Q 2 A2 A1 2 Force to be resisted 2 1 1 2 2 A2 A1 R FRx Example • A nozzle of diameter 20 mm is fitted to a pipe of diameter 60 mm. Find the force exerted by the nozzle on the water which is flowing through the pipe at the rate of 1.2 m3/min