Deep-Learning for Flow-Field Prediction of 3D Non-Axisymmetric Aero-Engine Nacelles
Author:
Affiliation:
1. Cranfield University Cranfield School of Aerospace Transport and Manufacturing
2. Rolls-Royce plc
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3307
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1. Design space dimensionality reduction through physics-based geometry re-parameterization
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5. Aerodynamic Design of a Flying Wing Using Response Surface Methodology
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