Write a computer program to solve potential flow problem as in lecture 4 note. Modify the the Octave source code so that it can be used to solve the following potential flow problem: uniform flow (in horizontal, vertical and inclined flow) source flow (show the effect of different source strength) sink flow (show the effect of different sink strength) superimpose uniform + source superimpose uniform + sink Flow past half Rankine oval Flow past Rankine oval Flow past non-rotating cylinder Flow past rotating cylinder of different vortex strength Plot the velocity and pressure contour for each problem listed above. Determine the stagnation point(s) for problem (6, 7, 8 and 9).

Write a computer program to solve potential flow problem as in lecture 4 note. Modify the the Octave source code so that it can be used to solve the following potential flow problem: 1. uniform flow (in horizontal, vertical and inclined flow) 2. source flow (show the effect of different source strength) 3. sink flow (show the effect of different sink strength) 4. superimpose uniform + source 5. superimpose uniform + sink 6. Flow past half Rankine oval 7. Flow past Rankine oval 8. Flow past non-rotating cylinder 9. Flow past rotating cylinder of different vortex strength Plot the velocity and pressure contour for each problem listed above. Determine the stagnation point(s) for problem (6, 7, 8 and 9). Write a report (to include introduction, method, source code, results and conclusion, and references) Write a computer program to solve potential flow problem as in lecture 4 note. Modify the the Octave source code so that it can be used to solve the following potential flow problem: 1. uniform flow (in horizontal, vertical and inclined flow) 2. source flow (show the effect of different source strength) 3. sink flow (show the effect of different sink strength) 4. superimpose uniform + source 5. superimpose uniform + sink 6. Flow past half Rankine oval 7. Flow past Rankine oval 8. Flow past non-rotating cylinder 9. Flow past rotating cylinder of different vortex strength Plot the velocity and pressure contour for each problem listed above. Determine the stagnation point(s) for problem (6, 7, 8 and 9). Write a report (to include introduction, method, source code, results and conclusion, and references)