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Asymmetric Oscillation Thrust Of Aeroacoustic Aircraft
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0 Geometries 0 Meshes 0 Simulation setups 0 ResultsAbout this project
This simulation explores the non-linear hydrodynamic/aerodynamic response of a body undergoing asymmetric sawtooth oscillations (fast forward, slow backward). The goal is study of the propulsion efficiency of experimental models. (DOI: 10.5281/zenodo.18047657). Technical Objectives: Analyze the Added Mass interaction during high-acceleration phases. Visualize Vortex Shedding asymmetry and its impact on net thrust. Investigate the "Biomimetic Oscillator" model as a macro-scale analog for quantum-hydrodynamic propulsion.
