Flutter Prediction Using Reduced-Order Modeling with Error Estimation
This paper presents a methodology for dynamic aeroelastic analysis of aircraft based on model order reduction with error estimation. A
...Efficient Flutter Prediction Using Reduced-Order Modeling
Cross Validation of Aerodynamic Shape Optimization Methodologies for Aircraft Wing-Body Optimization
Investigation into Aerodynamic Shape Optimization of Planar and Nonplanar Wings
Problems in three-dimensional aerodynamic shape optimization can produce complex design spaces due to the nonlinear physics of the
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Drag Minimization Based on the Navier–Stokes Equations Using a Newton–Krylov Approach
Approach to Aerodynamic Design Through Numerical Optimization
Multimodality and Global Optimization in Aerodynamic Design
Two optimization algorithms are presented that are capable of finding a global optimum in a computationally efficient manner: a gradient
...Numerical aerodynamic optimization incorporating laminar-turbulent transition prediction