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mach-aero-tutorial's Introduction

MACH-Aero Tutorials

Documentation Status

The tutorial site has moved! Please check out mdolab/MACH-Aero instead

This repository is kept for archival purposes only.

This repository contains step-by-step tutorials for MDO of aircraft configurations with high fidelity (MACH). The MACH framework is developed by the MDO Lab. It facilitates the aerodynamic design, analysis, and optimization of aircraft. The tutorial covers the basics needed to optimize the aerodynamic surface of a wing. It also includes an airfoil optimization example.

Tutorial documentation

You can either view the online tutorial or build the tutorial documentation locally. To generate the tutorial locally, open a terminal and enter the following commands:

$ cd mach_aero_tutorials/doc
$ make html

This generates html files in _build/html/. You can then open _build/html/index.html in your preferred browser to view the tutorial documentation.

Required Packages to build

  • Sphinx (1.6.6)

mach-aero-tutorial's People

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mach-aero-tutorial's Issues

Could slsqp get the same optimal CRM wing as snopt?

Could slsqp get the same optimal CRM wing as snopt do?

In the Aerodynamic Optimization docs of MACH_Aero_Tutorials, the optmization algorithm used
in the examlpe running script of a wing optimization is snopt. However, we couldn't get access of it for we don't purchase. So we change the optimization algorithm option by slspq. For CRM wing optimization, we couldn't get the same optimized wing as that obtained by snopt in your article. So, I wonder whether slsqp could get the same optimal CRM wing as mentioned in your article "Benchmarking Optimization Algorithms forWing Aerodynamic Design Optimization" by using these opensource codes? Or there is somthing wrong with my script?

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