Blade Airfoil Optimization with ANSYS
MAE 4700: Finite-Element Analysis Approaches
Situation
As a practice of this design process, optimize a given blade’s weight for specific Von Misses stresses and tip deflection by leveraging finite-element analysis methods in ANSYS Static Structural
Focus on parameters such as number of spars and ribs in the wing, thinning the skin, and altering the placement of the various components in the design.
Outcomes/ Constributions
Leveraged design parameter optimization in ANSYS Static Structural compute structural performance of 4 different wing blade geometries
Computed the model with 3 different numerical solution methodologies, specifically with different mesh refinement such as automated element optimization
Converged on a specific wing geometry, including ideal rib-spar thickness and placement, to reduce the blade’s weight by ~41.80% and operate within ideal conditions
Relevant Skills
ANSYS Structural, Design Optimization and Iterative Design, Defining Mathematical Models and Numerical Solutions, Report Writing