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Flugmechanik
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Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles
Development of Wing Structural Weight Equation for Active Aeroelastic Wing Technology
An Improved Process for the Generation of Drag Polars for use in Conceptual/Preliminary Design
An Automated Robust Process for Physics Based Aerodynamic Prediction
Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter
Development of Response Surface Equations for High-Speed Civil Transport Takeoff and Landing Noise
Aerodynamic Data Fusion Toward the Digital Twin Paradigm
Methodology for Probabilistic Analysis of Distributed Multidisciplinary Architecture
Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles
Efficient Aerodynamic Method for Interacting Lifting Surfaces over Long Distances