A matrix
Using the column-sum norm, compute the condition number and how many suspect digits would be generated by this matrix.
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Chapter 10 Solutions
EBK NUMERICAL METHODS FOR ENGINEERS
- * :Q4/B/ the value of X-bar is 0.987 1.5 2 2.5 2.5 O 2.5 X 0.398 O 2.5 2.5 0.857 0.55 0.254 0.5 0.487 1.06 0.65arrow_forwardQ1: * Q1 Calculate The Inverse Of The Matrix: [4 A= 2 -2 11 4 4 3 1 Add file Q2: * Using Green's theorem, evaluate the line integral (y- a)dr- (x +y°)dy, where the contour C encloses the sector of the circle with radius a lying in the first quadrant 0 = 1/2 R >-0 aarrow_forwardQ4/B/ the value of X-bai Q4/ For the figure below, all 0.987 dimensions in inch. A/The total O 2.5 Area : * O 0.857 O 0.254 y 0.398 O 1.06 1.5 O 2 0.65 2.5 0.5 2.5 O 0.487 0.55 2.5 2.5 Other: 3.arrow_forward
- Q2.The numerical solution of the Falknar-Scan Equation f' 0.0 0.0000000 0.000000 f" 0.363600 f + ff + B[1- (f )’]= 0 0.2 0.0093914 0.093905 0.4 0.0375492 0.187605 0.6 0.0843856 0.280575 0.355306 0.327254 0.301734 0.291190 about a plate with pressure gradient are given in Table. Eree stream velocity of air is. 10 m/s. 0.8 0.1496745 0.371963 1.0 0.2329900 0.460632 1.2 0.3336572 0.545246 0.284379 0.270565 Calculate: 1.4 0.4507234 0.624386 0.269692 1.6 0.5829560 0.696699 1.8 0.7288718 0.761057 2.0 0.8867962 0.766694 0.252487 0.240445 a) Boundary laver thickness, 8(x), dispalecement thickness &*(x) and the 0.225669 local friction coefficient. C (x). b) Drag force acting on the plate with 80 in length and 40 cm in width 2.2 1.0549463 0.793303 2.4 1.2315267 0.811065 0.210580 0.167561 2.6 1.4148231 0.830601 0.128613 Note: The density and viscosity of air is 1.12 kg/m and 1.56x10-s m²/s respectively. f' =u/U 2.8 1.6032823 0.852875 3.0 1.7955666 0.879054 0.095114 0.067711 0.046370 3.2 1.9905796…arrow_forwardFind the value of the variables a and b of the given linear equation below. a + b= 2 2a + b = 1 За + 2b %3D 3arrow_forwardIn the Blasius equation stream function: j is a dímensionless plane p(x, y) f(n) VDUX Values of f are not given in Table 7.1, but one published value is f(2.0) = 0.6500. Consider airflow at 6 m/s, 20°C, and 1 atm past a flat plate. Atx= 1 m, estimate (a) the height y; (b) the velocity, and (c) the stream function at 7= 2.0.arrow_forward
- The dependence of the tensions t (units: N) in a structure on the external forces f (units: N) follows the linear system Ct=f, where both t and f are 5 by 1 column vectors. The coefficient matrix C has been determined to be [ 11 14 20 -5 -19 ] -5 7 -3 5 -6 4 -5 13 -2 -10 0 0 0 12 -10 0 0 0 0 14 By how many N would the external force f2 need to be decreased (while all other external forces stay the same) in order to decrease the tension t3 by 94 N?arrow_forwardResolve for the x and y component of F3. y F3%3D650 N 3) F, = 750 N %3D 45° F = 900 N X component of F3: [Choose] y component of F3: [ Choose ]arrow_forwardFix my MATLAB code. % Define unknown quantities in x-y system % abc = Acceleration of B wrt C on beam CD in i direction % vbc = Velocity of B wrt C on beam CD in i direction % xacd = Angular acceleration of beam CD in k direction % xvcd = Angular velocity of beam CD in k direction syms abc vbc xacd xvcd; % Create Unit Vectors in x-y coordinates i = [1,0,0]; j = [0,1,0]; k = [0,0,1]; % Create Unit Vectors in X-Y coordinates (R is rotation Matrix) Theta = 150; % Angle from X-axis to x-axis R = [[cosd(Theta),-sind(Theta), 0]; ... [sind(Theta), cosd(Theta), 0]; [0, 0, 1]]; XYZ = R*[i;j;k]; I = XYZ(1,:); J = XYZ(2,:); K = XYZ(3,:); % Set known quantities for Beam AB (no slider connection). xVab = -2.5*K; % Angular Velocity of Beam AB xAab = -3*K; % Angular Acceleration of Beam AB Rba = 0.2*(cosd(135)*I + sind(135)*J ); % Vector from A to B in X-Y % Calculate velocity and acceleration of point B % due to rotation of Beam AB (no slider connection). Vb1 = cross(xVab,Rba); Ab1 =…arrow_forward
- Fill in each of the following blanks with the appropriate word: If the displacement model used in the derivation of the element stiffess matrices is also used to derive the element mass matrices, the resulting mass matrix is called __ mass matrix.arrow_forward(b) A beam is subjected to a linearly increasing distributed load. The elastic curve (deflection) is shown in the figure. The equation to find the maximum deflection is given below. Create a matlab code where you can calculate the maximum deflection (dy/dx=0) using the bisection method. Use initial guesses of 1 and 4, L= 6.46 m, E = 59000 kN/cm2, I=35000 cm4, and w0= 2.5 kN/cm. What will be the value of x (location of maximum deflection) after 14 bisection iteration? wo -23 +2L?x³ – L^x) 120EIL dy wo (-5x4 + 6L²a² – Lª) da 120EIL Choices 1.4445 O 2.6001 O4.3335 O 2.889arrow_forwardQuestion 10 The dimensions of an augmented matrix is 4 x 6. The corresponding system of linear equations has how many variables and how many equations? O 4 variables, 6 equations 5 variables, 4 equations O 6 variables, 3 equations 6 variables, 4 equationsarrow_forward
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