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CAD-CAE Integration for Wing Optimization by OSCARDELTA is a document available to read on EtoBox.

What is CAD-CAE Integration for Wing Optimization about?

This document describes a framework for optimizing wing design using multidisciplinary CAD-CAE integration. The framework involves parametric CAD modeling, aerodynamic load calculation, finite element analysis, and structural sizing. A bi-level optimization approach is used, with the inner level optimizing structural element thicknesses and the outer level optimizing the wing planform shape to minimize weight while maintaining lift-to-drag ratio. The process automates data exchange between Siemens NX, VORLA

Author

OSCARDELTA

Language

EN