Repeat Example 30.3, but for
To calculate: The temperature distribution of a long, thin aluminum rod with the given properties (refer Example 30.3, in the text book) when the rod is initially at
Answer to Problem 5P
Solution: The temperature distribution is,
Explanation of Solution
Given Information:
Consider, time is represented by variable t.
Length of the rod is 10 cm.
Here,
At,
Constant
Formula used:
At boundary node
From Crank Nicolson method, the difference equation for the nodes (except first and the last node) is expressed as,
Here,
Calculation:
For the first step at
Difference equation at node
Substitute
Since,
Therefore, the difference equations for node
Further, the system of equations (2), (3),(4), (5), (6), (7), (8), and (9) can be written in matrix form as,
Thus,
Execute the following code in MATLAB to evaluate the results in the above matrix equation
The output values thus obtained are:
Therefore,
Furthermore, for the second step to get the values at
Thus, solve as,
Execute the following code in MATLAB to evaluate the results in the above matrix equation
The output values thus obtained are:
Therefore,
Want to see more full solutions like this?
Chapter 30 Solutions
EBK NUMERICAL METHODS FOR ENGINEERS
Additional Engineering Textbook Solutions
APPLIED STAT.IN BUS.+ECONOMICS
Elementary Statistics: Picturing the World (7th Edition)
Finite Mathematics for Business, Economics, Life Sciences and Social Sciences
Elementary and Intermediate Algebra: Concepts and Applications (7th Edition)
College Algebra Essentials (5th Edition)
Intro Stats, Books a la Carte Edition (5th Edition)
- Calculate the stiffness matrix for the Q8 element shown below. Make use of the shape functions in natural coordinates and the Jacobian calculated in previous problems. Use 2x2 Gaussian numerical integration. Use plane strain conditions (for unit thickness) with E=200E9 (MPa) and nu=0.25. I have attached my matlab code below. Please look thru it and correct it. Thanks. u=sym('u') %%ztav=sym('v') %%eta x1=1x2=2x3=3.5x4=3.6x5=4.0x6=2.3x7=1.2x8=0.8 y1=1y2=1y3=1.3y4=2.3y5=3.3y6=3.2y7=3.0y8=2.0X=[x1;x2;x3;x4;x5;x6;x7;x8]Y=[y1;y2;y3;y4;y5;y6;y7;y8]%% diff of ztaDN1Du=1/4*(1-v)*(2*u+v);DN2Du=-u*(1-v);DN3Du=1/4*(1-v)*(2*u-v);DN4Du=1/2*(1-v^2);DN5Du=1/4*(1+v)*(2*u+v);DN6Du=-u*(1+v);DN7Du=1/4*(1+v)*(2*u-v);DN8Du=-1/2*(1-v^2); %% diff of etaDN1Dv=1/4*(1-u)*(2*v+u);DN2Dv=-1/2*(1-u^2);DN3Dv=1/4*(1+u)*(2*v-u);DN4Dv=-v*(1+u);DN5Dv=1/4*(1+u)*(2*v+u);DN6Dv=1/2*(1-u^2);DN7Dv=1/4*(1-u)*(2*v+u);DN8Dv=-v*(1-u);%% find dx/du dx/dv, dy/du and dy/dva=[DN1Du, DN2Du, DN3Du, DN4Du, DN5Du, DN6Du,DN7Du,…arrow_forwardFor the figure shown below (not to scale)... (a) Write equations for the internal forces at J (axial (F), shear (V), and bending (M)) in terms of only P and a. (b) Graph your equations as functions of P, using a =45°, from 0arrow_forwardDraw a rough graph & estimate the results just need an idea in very short time plz.arrow_forwardIn the Fig. 2 below, let Ki = K2 = K and ti = t=t. %3D T -T X Fig. 2 (a) Let T= 0 °C and T= 200 °C. Solve for T: and unknown rates of heat flow in term of k and t. MEC_AMO_TEM_035_02 Page 2 of 11 Finite Element Analysis (MECH 0016.1) – Spring - 2021 -Assignment 2-QP (b) Let T- 400 °C and let fs have the prescribed value f. What are the unknowns? Solve for them in term of K, t, and f.arrow_forwardCalculate the stiffness matrix for the Q8 element shown below. Make use of the shape functions in natural coordinates and the Jacobian calculated in previous problems. Use 2x2 Gaussian numerical integration. Use plane strain conditions (for unit thickness) with E=200E9 (MPa) and nu=0.25. The final answers is F1= 0.18452e12. I have attached my matlab code below. Please look thru it and correct it. Thanks. u=sym('u') %%ztav=sym('v') %%eta x1=1x2=2x3=3.5x4=3.6x5=4.0x6=2.3x7=1.2x8=0.8 y1=1y2=1y3=1.3y4=2.3y5=3.3y6=3.2y7=3.0y8=2.0X=[x1;x2;x3;x4;x5;x6;x7;x8]Y=[y1;y2;y3;y4;y5;y6;y7;y8]%% diff of ztaDN1Du=1/4*(1-v)*(2*u+v);DN2Du=-u*(1-v);DN3Du=1/4*(1-v)*(2*u-v);DN4Du=1/2*(1-v^2);DN5Du=1/4*(1+v)*(2*u+v);DN6Du=-u*(1+v);DN7Du=1/4*(1+v)*(2*u-v);DN8Du=-1/2*(1-v^2); %% diff of etaDN1Dv=1/4*(1-u)*(2*v+u);DN2Dv=-1/2*(1-u^2);DN3Dv=1/4*(1+u)*(2*v-u);DN4Dv=-v*(1+u);DN5Dv=1/4*(1+u)*(2*v+u);DN6Dv=1/2*(1-u^2);DN7Dv=1/4*(1-u)*(2*v+u);DN8Dv=-v*(1-u);%% find dx/du dx/dv, dy/du and dy/dva=[DN1Du, DN2Du, DN3Du,…arrow_forwardPlease don't provide handwritten solution ....arrow_forward2. In class, we derived an expression for hR/RT for a gas that obeyed the Pressure Explicit Virial Expansion truncated after the third term. In class, we assumed that B and C were not functions of temperature. a. Please rework the derivation with B = B(T) and C = 0. b. Please continue the derivation under the assumption that B(T) = mT + b. Where m and b are the slope and y-intercept of a straight, respectively. %3Darrow_forward7:17 l *l O O 93 A cylindrical steel pressure vessel 400 mm in diameter with a wall thickness of 20 mm, is subjected to an internal pressure of 5 MN/m^2. (a) Determine the safe stress between the tangential and longitudinal sections in the steel. (b) To what value may the internal pressure be increased if the stress in the steel is limited to 120 MPa? (c) If the internal pressure were increased until the vessel burst, sketch the type of fracture that would occur. * Your answer.arrow_forward8. Consider an iron bar, of diameter 4cm and length 1m, with specific heat c = 0.437J/(g K), density p= 7.88 g/cm³, and thermal conductivity K = 0.836 W/(cm K). Suppose that the bar is insulated except at the ends, it is heated to a constant tem- perature of 5 degrees Celsius, and the ends are placed in an ice bath (0 degrees Celsius). Compute the temperature (accurate to 3 digits) at the midpoint of the bar after 20 minutes. (Warning: Be sure to use consistent units.)arrow_forwardSOLVE IN DIGITAL FORMATarrow_forwardA rectangular plate ABCD with base L = 283 mm and height H = 376 mm experiences the deformation illustrated below, resulting in the deformed plate shown by dotted lines. Determine the average shear strain y at the corner C when a = 3 mm, b = 4 mm, c = 4 mm, d = 4 mm, e = 3 mm and f = 3 mm. Assume small deformations. %Matlab input: L = 283; H = 376; a = 3; b = 4; C = 4; d = 4; e = 3; f = 3: y d B C H b A a Larrow_forwardsolve numerical completlyarrow_forwardarrow_back_iosSEE MORE QUESTIONSarrow_forward_ios
- 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