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Showing 1 to 5 of 5 for “"airfoil optimization"”.

  1. Viscous airfoil optimization using conformal mapping coefficients as design variables

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.

    mit Repository record for Viscous airfoil optimization using conformal mapping coefficients as design variables (opens in a new tab)

  2. Shape optimization of cambered airfoils using a genetic algorithm and a multipoint inverse method

    … thesis presents a process to optimize a cambered airfoil with the MATLAB genetic algorithm (GA) and a multipoint inverse method called PROFOIL. XFOIL was used to evaluate the aerodynamic performance of each airfoil. Data processing techniques and a custom penalty function were developed in order …

    uiuc Repository record for Shape optimization of cambered airfoils using a genetic algorithm and a multipoint inverse method (opens in a new tab)

  3. INTEGRATION OF PHYSICS-INFORMED APPROACHES WITH MACHINE LEARNING TECHNIQUES FOR AERODYNAMICS

    … various aspects of aerodynamics, including the optimization of airfoil designs, prediction of 2D flow fields, and refinement of flush air data sensing systems. By integrating machine learning algorithms with fundamental principles of physics, this research endeavors to enhance the understanding …

    nus Repository record for INTEGRATION OF PHYSICS-INFORMED APPROACHES WITH MACHINE LEARNING TECHNIQUES FOR AERODYNAMICS (opens in a new tab)

  4. Optimization of Wind Turbine Airfoils/Blades and Wind Farm Layouts

    <p>Shape optimization is widely used in the design of wind turbine blades. In this dissertation, a numerical optimization method called Genetic Algorithm (GA) is applied to address the shape optimization of wind turbine airfoils and blades. In recent years, the airfoil sections with blunt trailing …

    wustl Repository record for Optimization of Wind Turbine Airfoils/Blades and Wind Farm Layouts (opens in a new tab)

  5. Airfoil design framework for optimized boundary-layer integral parameters

    Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-04-12 without embargo terms

    uiuc Repository record for Airfoil design framework for optimized boundary-layer integral parameters (opens in a new tab)