1. AdflowADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.
2. dafoamDAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Gradient-based Design Optimization
3. MACH-AeroMACH: MDO of Aircraft Configurations with High fidelity
4. pygeopyGeo provides surface generation, FFD, and geometric constraints for the MACH framework.
5. openconceptOpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
6. OpenAeroStructOpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
7. pyoptsparsepyOptSparse is an object-oriented framework for formulating and solving nonlinear constrained optimization problems in an efficient, reusable, and portable manner.