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Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow

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Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow ( aerodynamic-design-nasa-rotor-67-non-uniform-inflow )

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Master Thesis Report Development of Salome 2D & 3D Meshing template and Grid Generator Plot of Pressure Coefficient (Cp) at a Span Position of Y = 7 -1.5 -1 -0.5 0 0.5 1 5 6 7 8 9 10 11 x Figure 6.18: Pressure Coefficient Plot of Salome Meshed Wing Slice of the mesh. In order to construct the format of the SU2 based mesh, the following information is required: • VTK Number for each Element Type • Connecting Nodes for a given Element ID • Element Counter • Nodal Coordinates • Node Counter • Marker Tag • No. of Marker Elements • Connecting Nodes for a given Element ID for each Boundary Marker For a 2D triangle and quad mesh, there is a total of 3 and 4 connecting nodes respectively. When the information is being transferred from SALOME to SU2, certain information such as the total number of elements has to be modified before they can be printed onto the SU2 based mesh. Within SALOME, the total number of elements for a 2D geometry includes the edge elements as well as the face elements. However, the SU2 based mesh only requires the face elements during the element generation process. Therefore, the edge elements are removed for the generation of the SU2 based mesh. As for a 3D geometry, only the volume type mesh is required. Therefore, the edge and face elements are removed during the generation of the SU2 based mesh. Specifically, they are removed from the total number of element counter as well as from the element generation process during the first part of the SU2 Mesh writing sequences. An illustration of the SU2 Mesh format template is presented in figure 6.19. 69 Pressure_Coefficient

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