Energy Conservation (Bernoulli’s Equation) Integration of Euler’s equation Bernoulli’s equation dp VdV gdz 0 V1 p2 V22 gz1 gz2 2 p1 Flow.
Download ReportTranscript Energy Conservation (Bernoulli’s Equation) Integration of Euler’s equation Bernoulli’s equation dp VdV gdz 0 V1 p2 V22 gz1 gz2 2 p1 Flow.
Energy Conservation (Bernoulli’s Equation) Integration of Euler’s equation Bernoulli’s equation 2 1 dp 2 2 VdV gdz 0 1 1 2 V1 p2 V22 gz1 gz2 2 2 p1 Flow work + kinetic energy + potential energy = constant Dx p Under the action of the pressure, the fluid element moves a distance Dx within time Dt A The work done per unit time DW/Dt (flow power) is P DW pADx p Dx A AV , Dt Dt Dt 1 DW work done per unit mass flow rate AV Dt p Energy Conservation (cont.) 2 V1 p2 V22 z1 z2 , where g (energyper unit weight) 2g 2g p1 It is valid for incompressible fluids, steady flow along a streamline, no energy loss due to friction, no heat transfer. Determine the velocity and mass flow rate of efflux from the circular hole (0.1 m dia.) at the bottom of the water tank (at this instant). The tank is open to the atmosphere and H=4 m p1 = p2, V1=0 Examples: 1 H V2 2 g ( z1 z 2 ) 2 gH 2 2 * 9.8 * 4 8.85(m / s ) m AV 1000* 69.5 (kg / s ) 4 (0.1) 2 (8.85) Energy Equation(cont.) Example: If the tank has a cross-sectional area of 1 m2, estimate the time required to drain the tank to level 2. 1 First, choose the control volume as enclosed by the dotted line. Specify h=h(t) as the water level as a function of time. h(t) From Bernoulli' s equation, V = 2gh 2 water height (m) 4 4 3 h( t ) 2 2.5e-007 dm Ahole V dt Ahole dh (0.1) 2 since m Atan k h, V 2 2 gh dt Atan k 1 From mass conservation, dh 0.0443 h , dt 1 dh 0.0443dt, integrate h h(t) = H 0.0215t, h 0, tdrain 93 sec. 0 0 0 20 40 60 t time (sec.) 80 100 100 Energy conservation (cont.) Energy added, hA (ex. pump, compressor) Generalized energy concept: p1 p2 V1 z1 2g hL loss through valves 2 V2 z2 2g 2 Energy extracted, hE (ex. turbine, windmill) Energy loss, hL (ex. friction, valve, expansion) heat exchanger hA hE turbine pump hL, friction loss through pipes condenser hL loss through elbows Energy conservation(cont.) 2 V1 p2 V22 ExtendedBernoulli's equation, z1 hA hE hL z2 2g 2g p1 Examples: Determine the efficiency of the pump if the power input of the motor is measured to be 1.5 hp. It is known that the pump delivers 300 gal/min of water. 6-in dia. pipe 4-in dia.pipe hE=hL=0, z1=z2 2 1 Q=300 gal/min=0.667 ft3/s=AV pump V1=Q/A1=3.33 ft/s zo V2=Q/A2=7.54 ft/s Z=15 in kinetic energy head gain V22 V12 (7.54)2 (3.33)2 0.71 ft, 2g 2 * 32.2 Mercury (m=844.9 lb/ft3) water (w=62.4 lb/ft3) 1 hp=550 lb-ft/s p1 w zo m z p2 w zo w z p2 p1 ( m w )z (844.9 62.4) * 1.25 97813 . lb / ft 2 Energy conservation (cont.) Example (cont.) Pressure head gain: p2 p1 w 97813 . 15.67 ( ft ) 62.4 pump work hA p2 p1 w V22 V12 16.38( ft ) 2g Flow power delivered by pump P = w QhA (62.4)(0.667)(16.38) 681.7( ft lb / s) 1hp 550 ft lb / s P 1.24 hp Efficiency = P Pinput 1.24 0.827 82.7% 1.5 Frictional losses in piping system 2 V1 p2 V22 ExtendedBernoulli's equation, z1 hA hE hL z2 2g 2g p1 p2 Dp hL frictionalhead loss P p1 1 P2 Consider a laminar, fully developed circular pipe flow R: radius, D: diameter L: pipe length w: wall shear stress [ p ( p dp)](R 2 ) w (2R)dx, w p P+dp Darcy’s Equation: Pressure force balances frictional force dp 2 w dx, integrate from 1 to 2 R Dp p1 p2 4 hL w g F V I LL IV F LI f F K f HK G J H D 2H g2 g K D D 2 2 22 where f is defined as frictional factor characterizing f V F I f V F I w G J 44 K 22 Kpressure loss due to pipe wall shear stress H H When the pipe flow is laminar, it can be shown (not here) that f 64 VD , by recognizing that Re , as Reynolds number VD 64 , frictional factor is a function of the Reynolds number Re Similarly, for a turbulent flow, f = function of Reynolds number also Therefore, f f F(Re). Another parameter that influences the friction is the surface roughness as relativeto the pipe diameter F I H K D . (Re, :) Pipe frictional factor is a function of pipe Reynolds Such that f fFF Re, DD number and the relative roughness of pipe. This relation is sketched in the Moody diagram as shown in the following page. The diagram shows f as a function of the Reynolds number (Re), with a series of parametric curves related to the relative roughness F I. HD K Energy Conservation (cont.) Energy: E=U(internal thermal energy)+Emech (mechanical energy) =U+KE(kinetic energy)+PE(potential energy) Work: W=Wext(external work)+Wflow(flow work) Heat: Q heat transfer via conduction, convection & radiation dE=dQ-dW, dQ>0 net heat transfer in dE>0 energy increase and vice versa dW>0, does positive work at the expense of decreasing energy, dE<0 U=mu, u(internal energy per unit mass), KE=(1/2)mV2, PE=mgz Wflow=m(p/) F I G HJ K V2 p P Energy flow rate: m(u + gz ) plus Flow work rate m 2 V2 p V2 Flow energy in m in (u gz )in , Energy out = m out (u gz )out 2 2 p Their difference is due to external heat transfer and work done on flow Energy Conservation (cont.) p Heat in q=dQ/dt 2 V min (u gz)in 2 V2 m in (u gz )out 2 p Work out dW/dt From mass conservation: m in m out m From the First law of Thermodynamics (Energy Conservation): dQ p V2 p V2 dW m (u gz )in m (u gz )out , or dt 2 2 dt dQ V2 V2 dW m (h gz )in m (h gz )out dt 2 2 dt p where h u is defined as "enthaply" Energy Conservation(cont.) Example: Superheated water vapor is entering the steam turbine with a mass flow rate of 1 kg/s and exhausting as saturated steam as shown. Heat loss from the turbine is 10 kW under the following operating condition. Determine the power output of the turbine. From superheated vapor table: P=1.4 Mpa hin=3149.5 kJ/kg T=350 C V=80 m/s 2 2 dQ V V dW z=10 m m ( h gz ) m ( h gz ) 10 kw dt 2 in 2 out dW ( 10) (1)[(3149.5 2748.7) dt 80 2 50 2 (9.8)(10 5) ] 2(1000) 1000 10 400.8 1.95 0.049 P=0.5 Mpa 100% saturated steam 392.8(kW ) V=50 m/s z=5 m From saturated steam table: hout=2748.7 kJ/kg dt