Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
bartleby

Videos

Question
Book Icon
Chapter 14, Problem 29P
To determine

Calculate the global coefficient matrix of the two-element mesh.

Expert Solution & Answer
Check Mark

Answer to Problem 29P

The global coefficient matrix is [0.83330.66700.16670.6671.45830.3750.416700.3750.6250.250.16670.41670.250.833]_.

Explanation of Solution

Calculation:

Refer to Figure 14-62 in the textbook for the two-element mesh.

For element 1, local numbering 1-2-3 corresponds to global numbering 1-2-4.

From Figure 14.62, the given values for element 1 are,

x1=0,x2=1,x3=2,y1=1,y2=0,andy3=2.

Calculate the value of P1.

P1=y2y3=02=2

Calculate the value of P2.

P2=y3y1=21=1

Calculate the value of P3.

P3=y1y2=10=1

Calculate the value of Q1.

Q1=x3x2=21=1

Calculate the value of Q2.

Q2=x1x3=02=2

Calculate the value of Q3.

Q3=x2x1=10=1

Consider the expression for the area A.

A=12(P2Q3P3Q2)        (1)

Substitute 1 for P2, 1 for P3, 2 for Q2, and 1 for Q3 in Equation (1).

A=12[((1)(1)(1)(2))]=32

Write the expression for co-efficient Cij.

Cij=14A[PiPj+QiQj]        (2)

By using Equation (2), the coefficient values C11,C12,C13,C21,C22,C23,C31,C32,andC33 are calculated as 56,46,16,46,56,16,16,16,and26 respectively.

Write the expression of the element coefficient matrix C(1).

C(1)=[C11C12C13C21C22C23C31C32C33]

Substitute 56 for C11, 46 for C12, 16 for C13, 46 for C21, 56 for C22, 16 for C23, 16 for C31, 16 for C32, and 26 for C33.

C(1)=[564616465616161626]

For element 2, local numbering 1-2-3 corresponds to global numbering 4-2-3.

From Figure 14.62, the given values for element 2 are,

x1=2,x2=1,x3=3,y1=2,y2=0,andy3=0.

Calculate the value of P1.

P1=y2y3=00=0

Calculate the value of P2.

P2=y3y1=02=2

Calculate the value of P3.

P3=y1y2=20=2

Calculate the value of Q1.

Q1=x3x2=31=2

Calculate the value of Q2.

Q2=x1x3=23=1

Calculate the value of Q3.

Q3=x2x1=12=1

Substitute 2 for P2, 2 for P3, 1 for Q2, and 1 for Q3 in Equation (1) to find area A.

A=12[((2)(1)(2)(1))]=2

By using Equation (2), the coefficient values C11,C12,C13,C21,C22,C23,C31,C32,andC33 are calculated as 48,28,28,28,58,38,28,38,and58 respectively.

Write the expression of the element coefficient matrix C(2).

C(2)=[C11C12C13C21C22C23C31C32C33]

Substitute 48 for C11, 28 for C12, 28 for C13, 28 for C21, 58 for C22, 38 for C23, 28 for C31, 38 for C32, and 58 for C33.

C(2)=[482828285838283858]

Calculate the global coefficient matrix.

C=[C11(1)C12(1)0C13(1)C12(1)C22(1)+C22(2)C23(2)C23(1)+C21(2)0C23(2)C33(2)C31(2)C13(1)C23(1)+C21(2)C31(2)C33(1)+C11(2)]=[0.83330.66700.16670.6671.45830.3750.416700.3750.6250.250.16670.41670.250.833]

Conclusion:

Thus, the global coefficient matrix is [0.83330.66700.16670.6671.45830.3750.416700.3750.6250.250.16670.41670.250.833]_.

Want to see more full solutions like this?

Subscribe now to access step-by-step solutions to millions of textbook problems written by subject matter experts!
Students have asked these similar questions
Derive the equation below ah ap ax 12μ ax, +( ah ap ay 12μ ay Where P P (x, y) is the oil film pressure. 1..ah 2 ax
Can you determine the eignevalues by hand?
Monthly exam 13 2021-2022 Power plant Time: 1.5 Hrs Q1. A The gas-turbine cycle shown in Fig. is used as an automotive engine. In the first turbine, the gas expands to pressure Ps, just low enough for this turbine to drive the compressor. The gas is then expanded through the second turbine connected to the drive wheels. The data for the engine are shown in the figure, and assume that all processes are ideal. Determine the intermediate pressure Ps, the net specific work output of the engine, and the mass flow rate through the engine. Find also the air temperature entering the burner T3 and the thermal efficiency of the engine. Exhaust Air intake Φ www Regenerator www Bumer Compressor Turbine Power turbine et 150 kW Wompressor P₁ = 100 kPa T₁ = 300 K PP₁ =60 P-100 kPa T₁ = 1600 K Q2. On the basis of a cold air-standard analysis, show that the thermal efficiency of an ideal regenerative gas turbine can be expressed as 77 = 1- where - () () гp is the compressor pressure ratio, and T₁ and…
Knowledge Booster
Background pattern image
Mechanical Engineering
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
SEE MORE QUESTIONS
Recommended textbooks for you
Text book image
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Text book image
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Text book image
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Text book image
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Text book image
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Text book image
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
Ficks First and Second Law for diffusion (mass transport); Author: Taylor Sparks;https://www.youtube.com/watch?v=c3KMpkmZWyo;License: Standard Youtube License