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Master Thesis Report Introduction Chapter 2 of this report will present a short summary of the literature study. This will include a study on the comparison between embedded and podded engine configurations, a cycle analysis on the effect of boundary layer ingestion on the thermodynamic and propulsive efficiency, a study on blade parametrisation, construction, loss mechanism and performance characterisation of the rotor blade and finally a literature review on the capabilities and function of SU2 Computational Fluid Dynamics (CFD) Code. After the literature review, chapter 3 of the report will specifically present on the overall research objective, goal and the scope of this thesis work. Chapter 4 of the report will then focus on the actual methodology used to parametrise and reconstruct the NASA Rotor 67. This is followed by a presentation on the design trend of the rotor blade. In order to validate the blade reconstruction method, Chapter 5 of the report will touch on the results of the 2D blade profile simulation. Since a part of the research work was focused on coupling Salome, an open source meshing software onto the blade modeller, a part of the 2D CFD simulation results will present on the comparison of per- formances results of the same profile under the use of different meshing software. Chapter 6 of the report will then touch on the development of meshing template for both 2D and 3D blade profiles in SALOME as well as the coupling of SALOME to the blade modeller. Chapter 7 of the report will then present on the 3D boundary conditions and simulation results for both uniform and non uniform inflow condition. Finally, Chapter 8 of the report will present on the conclusion and recommendations from this research. 3PDF Image | Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow
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