Abstract
Abstract The verification of a Direct Numerical Simulation code is carried out using the Method of Manufactured Solutions. Numerical results from the code are also compared with experimental and Linear Stability Theory results in a boundary layer over an airfoil. Displacement thickness, momentum thickness and shape factor are used to measure the boundary layer. Comparisons considering the amplitude of the velocity disturbance caused by two-dimensional Tollmien–Schlichting waves are also made. The results show the verification and validation of the Direct Numerical Simulation code.
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