3. Dynamics and control of two tank in series Thefollowing system is given: A water storage Tank 1 in whichwater is stored at atmospheric pressure and distributed by gravityflow in a downfeed in the same type water storage Tank 2.Where: h1, h2 is water level(m), S1, S2 is squared area of botomof the tank cilinders (m²),F1 in/F2in-water inflow, F1/F2out- wateroutflow(m³/h), k1, k: Valve constant (m²5/h), pipe length is2.5ommited.F1inh1S1Tank 1k1h2F1 outF2 inS2k2F2 outTank 23.1 Describe the dynamic behavior of a tank 1 in terms ofordinary differential equations.3.2 Describe the dynamic behavior of the level h2/ tank 2/, dueto the input flow Flin. in terms of ordinary differential equations.3.3 Determine the transfer function of the level h2 as output,due to the input flow Flin.3.4 Select the strategy to control the plant / level control system /with Flin as control action and output- level h2/ tank 2 /Design the proper instrumentation and Sketch the P&IDinstrumentation diagram/.

Given: To find: ODE of tank 1 ODE of tank 2 Transfer function

3. Dynamics and control of two tank in series The following system is given: A water storage Tank 1 in which water is stored at atmospheric pressure and distributed by gravity flow in a downfeed in the same type water storage Tank 2. Where: h1, h2 is water level(m), S1, S2 is squared area of botom of the tank cilinders (m²),F1 in/F2in-water inflow, F1/F2 out- water outflow(m³/h), kl, k: Valve constant (m25/h), pipe length is ommited.

3. Dynamics and control of two tank in series The following system is given: A water storage Tank 1 in which water is stored at atmospheric pressure and distributed by gravity flow in a downfeed in the same type water storage Tank 2. Where: h1, h2 is water level(m), S1, S2 is squared area of botom of the tank cilinders (m²),F1 in/F2in-water inflow, F1/F2 out- water outflow(m³/h), kl, k: Valve constant (m25/h), pipe length is ommited.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

Cakulate the time rate of change of air density during expiration Assume that the lung (Fig. 3.11) has a total volume of 6000 ml, the diameter of the trachea is 18 mm, the airflow velocity out of the trachea is 20 cm/s, and the density of air is 1.225 kg/m. Also assume that lung volume is decreasing at a rate of 100 mL/s. Hello sir, I want the same solution, but in a detailed way and mention his data, a question, and a solution in detailing mathematics without words. Solution We will start from Eq. (3.24) because we are asked for the time rate of change of density. We are asked to find the time rate of change of air density; this suggests that Example 3.5 condis tions are representing a nonsteady flow scenario. In addition, we were told what the rate of change in the lung volume is during this procedure, further supporting the use of Eq. (3.24). pdV+ (3.24 ams Assume that at the instant in time that we are measuring the system, density is uniform within the volume of interest. This…
2. Prove the following equations for a simple compressible system: (a) du = cy dT + dv K (b) dh= cp dT + (v – aTv) dp KCy (c) ds aT dp + dv aTv %3D (d) da=-(apv + s) dT + kpv dp
K:55)
conditioning
Q5: A small tank of Helium gas, its pressure is 15.5 bar and its temerature is 293 K (Kelvin) with volume of 0.02 m³. This small tank used to fill out a balloon. So what is the volume of this balloon if it filled at a pressure of 1 bar and a temperature of 110' F (Fahrenheit)?
Q2: if we have three fluids with different properties as listed below: - {fluid 1: has weight, which is greater than water 7.5 times}. {fluid 2: has the specific volume equal to 0.1}. {fluid 3: has uniform distribution velocity through the section of flow}. Now answer the following: - For fluid 1, find the weight density and mass density. Determine the types of fluid 2 and 3.
fet), force force, f 10 Newt. m2 f k, 10sec m, = 10 kg, ma= 20 kg , b= 20 Newton m/sec k, = 30 Newton kz = 60 Newton z, and z are measured with respeet to eguilibrium conditions and all imitial conditions are zero, 1) Write the Newton's second Lau for m, amd m2 2) Derive a statespace represrentation of the conditions : eystem fallowing 2a) only z, is measured 26) only z, is measured 2c) (2,-z,) is measured. un der 3) Derive the following transfor fumetione fG) z,(5) Go G,6) ? G6) ? 4) Describe a mechanical device that can be used to implement the external force fee) as shoun'a bove. 5) Using (Csim) function of MATLAB, plot z,(t), 2, (t)- =, (+)] Zz (t) and
A1) Floodgates, also known as stop gates, are adjustable gates that restrict the flow of water in flood barriers, reservoirs, rivers, and stream systems. Floodgates prevent river water from backing up into cities during high water levels. 5 m 160° B Figure 1: Floodgate As an aerospace engineer with a solid foundation in fluid mechanics, you would like to propose a temporary design solution to mitigate the damage or disruption of a nearby airport runway flood. The floodgate is 3 m wide and 5 m long, with a solid gate (AB) hinged at point B and restrained by a force-pulley mechanism at point A. The value of mass P is 2500 kg. Assume the density of water is 1000 kg/m. a) Draw the free body diagram of the floodgates system. b) Calculate the depth of water assuming this rectangular gate is in equilibrium, ignoring the weight of the gate. c) Repeat the calculation as in (a), including the weight of the 5-cm-thick steel (SG = 7.8) gate. d) Suppose the length of the gate AB is doubled; what…
4.7 Find the power required to pump water from one tank to another, as shown in Fig. 4.31. The discharge through the pump is 30 L/s. Neglect all the losses. d = 50 mm Z3 =15m d= 10 mm 2 = 3m 21 = 5m Fig. 4.31 [Ans: 6.445 kW]
Fluid Mechanics: Concept Question: From Bernoullis equation, if you have point A and point B, where point A is at a higher elevation than point B, lets say Z1 and Z2 respectively - You have a pump running the fluid from point B to point A , i.e. against gravity. I understand the following: Pressure losses, h, moves in the same direction as your flow, v, and your friction, f, moves opposite to your flow, always. So the head loss AS A RESULT OF FRICTION from Z2 to Z1, will be negative or positive? I assume negative, and the value of the aforementioned head loss will be positive in the bernoulli equation on the side of the equation involving A , as this is the direction the flow is moving towards. Hence my question: So the head loss AS A RESULT OF FRICTION from Z2 to Z1, will be negative or positive?
A wind turbine gives the following data: Blade length= 55.5 m. Wind speed = 11 m/s Air density = 1.227 Kg/m3 Power coefficient = 0.55 Assuming equal efficiencies for gearbox and generator, If the Power output from wind turbine, P is 2.1 MW, then find a) Rotor Power Output, P- in M (* b) Wind Power, Pw in MW (: C) Efficiency of Generator Rotor Power Output, Pr in MW
Need help with engineering problem. Match the RTT term with its explanation: A: ddt(∫CVβρdᏉ) B: ∫CSβρVcosθdAout C: ∫CSβρVcosθdAin A. B. C. Match one of the following answers below to each letter. A change within the control volume Outflow of B from the ontrol volume Inflow of B to the control volume