
(a)
The steady state, transient, free and forced responses for the following nonhomogenous equation

Answer to Problem 2.23P
Steady state response is 2.
Transient state response is
Free response is
Forced response is
Explanation of Solution
Given:
The given equation is as:
With initial conditions as follows:
Concept Used:
The given nonhomogenous equation is first transformed into the time domain using the Laplace transform as shown:
Taking Laplace of the above equation that is,
Now, the expression for
Therefore,
Now, in order to simplify the above equation, the partial fraction expansion could be used so that the expression becomes as:
Then, the inverse Laplace of
And for the free response the input would be taken zero or say the right-hand side part of the given equation is kept zero as shown:
Therefore,
For the forced response the initial conditions are kept zero such that:
Then the inverse of these two functions is calculated for finding the respective response.
Calculation:
The equation to be solved is as:
By taking the Laplace of this equation that is,
Therefore,
Using the partial fraction expansion, the transfer function could be simplified as shown below:
Now, on taking the inverse Laplace of the above transfer function, we get
Thus the above response consists of two parts, that is, the steady-state response and the transient state response.
Steady state response is 2.
Transient state response is
At zero initial conditions, using the partial fraction expansion
Therefore,
This is the forced response.
At zero input condition, using the partial fraction expansion.
Therefore,
This is the free response.
Conclusion:
Steady state response is 2.
Transient state response is
Free response is
Forced response is
(b)
The steady state, transient, free and forced responses for the following nonhomogenous equation

Answer to Problem 2.23P
Steady state response is
Transient state response is
Free response is
Forced response is
Explanation of Solution
Given:
The given equation is as:
With initial conditions as follows:
Concept Used:
The given nonhomogenous equation is first transformed into the time domain using the Laplace transform as shown:
Taking Laplace of the above equation that is,
Now, the expression for
Therefore,
Now, in order to simplify the above equation, the partial fraction expansion could be used so that the expression becomes as:
Then, the inverse Laplace of
And for the free response the input would be taken zero or say the right-hand side part of the given equation is kept zero as shown:
Therefore,
For the forced response the initial conditions are kept zero such that:
Then the inverse of these two functions is calculated for finding the respective response.
Calculation:
The equation to be solved is as:
By taking the Laplace of this equation that is,
Therefore,
Using the partial fraction expansion, the transfer function could be simplified as shown below:
Now, on taking the inverse Laplace of the above transfer function, we get
Thus the above response consists of two parts, that is, the steady-state response and the transient state response.
Steady state response is
At zero initial conditions, using the partial fraction expansion
Therefore,
This is the forced response.
At zero input condition, using the partial fraction expansion.
Therefore,
This is the free response.
Conclusion:
Steady state response is
Transient state response is
Free response is
Forced response is
(c)
The steady state, transient, free and forced responses for the following nonhomogenous equation

Answer to Problem 2.23P
Steady state response is
Transient state response is
Free response is
Forced response is
Explanation of Solution
Given:
The given equation is as:
With initial conditions as follows:
Concept Used:
The given nonhomogenous equation is first transformed into the time domain using the Laplace transform as shown:
Taking Laplace of the above equation that is,
Now, the expression for
Therefore,
Now, in order to simplify the above equation, the partial fraction expansion could be used so that the expression becomes as:
Then, the inverse Laplace of
And for the free response the input would be taken zero or say the right-hand side part of the given equation is kept zero as shown:
Therefore,
For the forced response the initial conditions are kept zero such that:
Then the inverse of these two functions is calculated for finding the respective response.
Calculation:
The equation to be solved is as:
By taking the Laplace of this equation that is,
Therefore,
Using the partial fraction expansion, the transfer function could be simplified as shown below:
Now, on taking the inverse Laplace of the above transfer function, we get
Thus the above response consists of two parts, that is, the steady-state response and the transient state response.
Steady state response is
Transient state response is
At zero initial conditions, using the partial fraction expansion.
Therefore,
This is the forced response.
At zero input condition, using the partial fraction expansion.
Therefore,
This is the free response.
Conclusion:
Steady state response is
Transient state response is
Free response is
Forced response is
(d)
The steady state, transient, free and forced responses for the following non homogenous equation

Answer to Problem 2.23P
Steady state response is
Transient state response is
Free response is
Forced response is
Explanation of Solution
Given:
The given equation is as:
With initial conditions as follows:
Concept Used:
The given nonhomogenous equation is first transformed into the time domain using the Laplace transform as shown:
Taking Laplace of the above equation that is,
Now, the expression for
Therefore,
Now, in order to simplify the above equation, the partial fraction expansion could be used so that the expression becomes as:
Then, the inverse Laplace of
And for the free response the input would be taken zero or say the right-hand side part of the given equation is kept zero as shown:
Therefore,
For the forced response the initial conditions are kept zero such that:
Then the inverse of these two functions is calculated for finding the respective response.
Calculation:
The equation to be solved is as:
By taking the Laplace of this equation that is,
Therefore,
Using the partial fraction expansion, the transfer function could be simplified as shown below:
Now, on taking the inverse Laplace of the above transfer function, we get
Thus the above response consists of two parts, that is, the steady-state response and the transient state response.
Steady state response is
Transient state response is
At zero initial conditions, using the partial fraction expansion.
Therefore,
This is the forced response.
At zero input condition, using the partial fraction expansion.
Therefore,
This is the free response.
Conclusion:
Steady state response is
Transient state response is
Free response is
Forced response is
Want to see more full solutions like this?
Chapter 2 Solutions
System Dynamics
- Temperature EXAMPLE 1: A diesel engine is fitted with a turbocharger, which comprises a radial compressor driven by a radial exhaust gas turbine. The air is drawn into the compressor at a pressure of 0.95 bar and at a temperature of 15°C, and is delivered to the engine at a pressure of 2.0 bar. The engine is operating on a gravimetric air/fuel ratio of 18: 1, and the exhaust leaves the engine at a temperature of 600°C and at a pressure of 1.8 bar; the turbine exhausts at 1.05 bar. The isentropic efficiencies of the compressor and T(K) turbine are 70 per cent and 80 per cent, respectively. Calculate (i) the temperature of the air leaving the compressor (ii) the temperature of the gases leaving the turbine (iii) the mechanical power loss in the turbocharger expressed as a percentage of the power generated in the turbine. Using the values of : Cpair = 1.01 kJ/kg K, Vair = 1.4 Cpex = 1.15 kJ/kg K, Yex = 1.33 and 2s с P2 Engine P3 W W₁ = mexpex (T3-TA) At W₁ = mair Cpex (T2-T₁) 4 P4…arrow_forwardProblem 8.28 Part A 10 of 10 ■Review The uniform crate resting on the dolly has a mass of 530 kg and mass center at G as shown in (Figure 1). If the front casters contact a high step, and the coefficient of static friction between the crate and the dolly is μs = 0.45, determine the greatest force P that can be applied without causing motion of the crate. The dolly does not move. Express your answer to three significant figures and include the appropriate units. Figure -0.5 m- 0.6 m 0.3 m 0.1 m B 0.4 m 0.3 m > ☐ P = 1210 Submit о ΜΑ N Previous Answers Request Answer × Incorrect; Try Again 1 of 1 < Return to Assignment Provide Feedback ?arrow_forwardQ1: For the system shown in Fig. 6.7, the following data are applicable P1 = 7 bar Q=0.002 m3/sec Pipe: total length 15m and ID 38mm Oil: SG-0.90 and kinematic viscosity (v-0.0001 m2/s) Solve for P2 in units of bars. Motor OH Pump Breather P1 Pipe length = 3m 90' elbow ☐ 38 mm (ID) Pipe length = 2m P2 Load force Pipe length 4 m = Pipe length=6m 90' elbowarrow_forward
- using the three moment theorem please find the moments about B, C and Darrow_forwardA viscous fluid flows in a 0.10-m-diameter pipe such that its velocity measured 0.010 m away from the pipe wall is 0.9 m/s. If the flow is laminar, determine (a) the centerline velocity and (b) the flowrate. (a) Vi (b) Q = i m/s × 103 m³/sarrow_forwardThis is an old exam review question please help.arrow_forward
- 3. The volumetric flow rate of air through a duct transition of the type shown in Table 12-9b (rectangular with two parallel sides) is 2 m3/s. The duct before the transition issquare, with a height of 50 cm. The expansion ratio across the transition is 4 (i.e., theduct area after the transition is 4 times greater than the duct area before the transition).a) Determine the pressure loss (in Pa) across the transition if the exit from the duct isabrupt (i.e., the diverging angle of the transition is 180º).b) Determine the percentage reduction in pressure loss for a transition diverging angleof 20º compared to the one in part (a).c) The head HVAC engineer requires the pressure loss across the transition to bereduced to less than 50% of the pressure loss for an abrupt exit (i.e., the case in part(a)), and suggests a transition diverging angle of 45º. Will this new diverging angleachieve the required reduction in pressure loss? Justify your answer.d) For a transition diverging angle of 90º,…arrow_forwardThe wheel shown is made of 2 rings and 8 rods. The otter ring weighs 100 lbs, the inner ring weighs 15 lbs,and each of the rods weighs 20 lbs. Find the moment of inertia of the wheel about an axis that comes directlyout of the page through point A.arrow_forwardMini project You are an engineer working for a power systems company responsible for ensuring grid stability. Your team has recently observed low-frequency oscillations in the system following disturbances such as load changes, faults, and switching operations. These oscillations have led to voltage instability, frequency deviations, and, in severe cases, system blackouts. A task force has been formed to address this issue, and you have been assigned a critical role in developing a damping control strategy. Your objective is to analyze system performance, propose engineering solutions, and compare the effects of different damping approaches. Answer the following questions 1. Identify the Engineering Problem: - What is the fundamental issue affecting power grid stability? - How do low-frequency oscillations impact the system's reliability? - What parameters indicate system instability? 2. Assess the Current Status Using Equations and Calculations: - Given the characteristic roots of the…arrow_forward
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY





