Installation Aerodynamics of Aero-Engine Nacelles
Cranfield Individual Research Project
- Investigating installation aerodynamics using a Python-based propulsion-integration tool, applying iCST parametric geometry to model nacelle installation effects.
- Developing and benchmarking a pyOCC / OpenCASCADE geometry-generation workflow against commercial CAD output for accuracy and robustness.
Python · iCST · pyOCC · OpenCASCADE · OpenFOAM
