Figure 1 is a boundary layer velocity profiles developed on a flat plate. The data was measured by a hot-wire probe. The tabulated form of Figure 1 can be found from Table 1. Using the data, calculate the: a) Boundary layer thickness b) Displacement thickness c) Momentum thickness After that, please state that whether the boundary layer is laminar or turbulent. 6:% yx Exit Fullscreen \begin{tabular}{rr} y(mm) & u(m/s) \\ \hline 0.27 & 0.8279 \\ 0.37 & 1.1407 \\ 0.47 & 1.4736 \\ 0.57 & 1.8798 \\ 0.67 & 2.2766 \\ 0.76 & 2.6525 \\ 0.87 & 3.0467 \\ 0.97 & 3.417 \\ 1.07 & 3.7813 \\ 1.17 & 4.1294 \\ 1.27 & 4.4804 \\ 1.37 & 4.8128 \\ 1.46 & 5.1125 \end{tabular} \begin{tabular}{ll} 1.57 & 5.4591 \\ 1.67 & 5.8079 \\ 1.77 & 6.1036 \\ 1.87 & 6.4084 \\ 1.97 & 6.6936 \\ 2.07 & 6.9835 \\ 2.17 & 7.2691 \\ 2.27 & 7.5343 \\ 2.36 & 7.8141 \\ 2.46 & 8.0293 \\ 2.56 & 8.2717 \\ 2.67 & 8.512 \\ 2.76 & 8.7274 \\ 2.87 & 8.9918 \\ 2.97 & 9.1578 \\ 3.06 & 9.3425 \\ 3.16 & 9.5128 \\ 3.26 & 2.6224 \\ \hline \end{tabular} 6:2 \begin{tabular}{rr} 2.27 & 7.5343 \\ 2.36 & 7.8141 \\ 2.46 & 8.0293 \\ 2.56 & 8.2717 \\ 2.67 & 8.512 \\ 2.76 & 8.7274 \\ 2.87 & 8.9918 \\ 2.97 & 9.1578 \\ 3.06 & 9.3425 \\ 3.16 & 9.5128 \\ 3.26 & 9.6773 \\ 3.37 & 9.8412 \\ 3.46 & 9.9627 \\ 3.56 & 10.1048 \\ 3.66 & 10.2615 \\ 3.76 & 10.3861 \\ 3.87 & 10.5048 \\ 3.97 & 10.6012 \\ 4.06 & 10.6681 \\ 4.17 & 10.7949 \\ 4.27 & 10.8639 \\ 4.37 & 10.9432 \\ 4.46 & 10.9791 \\ 4.56 & 11.0393 \\ 4.67 & 11.0968 \\ 4.76 & 11.1367 \\ 4.87 & 11.1767 \\ 5.07 & 11.2669 \\ 5.27 & 11.3067 \\ 5.47 & 11.34 \\ 5.68 & 11.3973 \\ 5.88 & 11.409 \\ 6.29 & 11.4391 \\ 6.69 & 11.45 \\ 7.09 & 11.4607 \\ 7.49 & 11.4747 \\ 7.89 & 11.4767 \\ 9.91 & 11.4716 \\ 11.9 & 11.4718 \\ 14.9 & 11.4806 \\ 17.91 & 11.4775 \\ 19.91 & 11.4694 \\ \hline \end{tabular} 6:2 5.275.475.685.886.296.697.097.497.899.9111.914.917.9119.9111.308711.3411.397311.40911.439111.4511.460711.474711.476711.471611.471811.480611.477511.4694 24.911.4638 29.911.4722 34.9 11.474 Table 1