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