OpenAeroStruct | lightweight tool that performs aerostructural optimization

by mdolab Python Version: 2.7.1 License: Apache-2.0

X-Ray Key Features Code Snippets Community Discussions(1)Vulnerabilities Install Support

kandi X-RAY | OpenAeroStruct Summary

OpenAeroStruct is a Python library. OpenAeroStruct has no bugs, it has no vulnerabilities, it has build file available, it has a Permissive License and it has low support. You can install using 'pip install OpenAeroStruct' or download it from GitHub, PyPI.

OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.

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Support

OpenAeroStruct has a low active ecosystem.

It has 143 star(s) with 105 fork(s). There are 21 watchers for this library.

There were 1 major release(s) in the last 12 months.

There are 32 open issues and 136 have been closed. On average issues are closed in 277 days. There are 1 open pull requests and 0 closed requests.

It has a neutral sentiment in the developer community.

The latest version of OpenAeroStruct is 2.7.1

Quality

OpenAeroStruct has 0 bugs and 0 code smells.

Security

OpenAeroStruct has no vulnerabilities reported, and its dependent libraries have no vulnerabilities reported.

OpenAeroStruct code analysis shows 0 unresolved vulnerabilities.

There are 0 security hotspots that need review.

License

OpenAeroStruct is licensed under the Apache-2.0 License. This license is Permissive.

Permissive licenses have the least restrictions, and you can use them in most projects.

Reuse

OpenAeroStruct releases are available to install and integrate.

Deployable package is available in PyPI.

Build file is available. You can build the component from source.

Installation instructions are not available. Examples and code snippets are available.

Top functions reviewed by kandi - BETA

kandi has reviewed OpenAeroStruct and discovered the below as its top functions. This is intended to give you an instant insight into OpenAeroStruct implemented functionality, and help decide if they suit your requirements.

Generate a mesh from input dictionary
Add the chords to the mesh
Generate a crm mesh
Return the CRM points for a given wing
Compute the partials of a mesh
Compute the cross product of two vectors
Return unit vector of vec
Compute the surface components
Compute the cross between two arrays
Apply nonlinear constraints to the input tensor
Compute the reaction volume
Compute the panel forces
Compute the components of the graph
Solve nonlinear problem
Compute the partials of the grid
Compute transformation
Runs a test on the model
Setup the model
Compute the transition matrix
Calculate the energy of a grid
R Compute the polar pressure
Compute quadratic model
R Compute the polar ground effect
Generate surfaces from OpenV file
Generate documentation
Save the design to a movie

Get all kandi verified functions for this library.

OpenAeroStruct Key Features

No Key Features are available at this moment for OpenAeroStruct.

OpenAeroStruct Examples and Code Snippets

No Code Snippets are available at this moment for OpenAeroStruct.

Community Discussions

Trending Discussions on OpenAeroStruct

compute_totals returns the wrong total derivatives when approx_totals is not used

QUESTION

compute_totals returns the wrong total derivatives when approx_totals is not used

Asked 2020-Feb-18 at 17:34

I noticed that prob.compute_totals() returns a wrong answer when prob.model.approx_totals() is not specified before. Having the partial derivative manually defined or computed by finite differences doesn't change anything, the answer remains wrong when not calling prob.model.approx_totals() before. Also, the call to compute_totals is actually faster when approx_totals is called before, compared to when it's not. This seems counter-intuitive with manually defined partials, since approx_totals is supposed to add an unnecessary finite-difference computation.

Here is a MWE with the Sellar example taken from the OpenMDAO documentation. I also noticed the same behaviour in OpenAeroStruct, even though the differences are smaller than in this example.

...

ANSWER

Answered 2020-Feb-18 at 17:34

In this example, the problem is that you have a cycle in SellarMDA, but the model does not contain a linear solver that can compute the total derivatives across the cycle. One way you can check on this is to run "openmdao check myfilename.py" at the command-line. I ran it on your model, and got the following warnings:

Source https://stackoverflow.com/questions/60285698

Community Discussions, Code Snippets contain sources that include Stack Exchange Network

Vulnerabilities

No vulnerabilities reported

Install OpenAeroStruct

You can install using 'pip install OpenAeroStruct' or download it from GitHub, PyPI.
You can use OpenAeroStruct like any standard Python library. You will need to make sure that you have a development environment consisting of a Python distribution including header files, a compiler, pip, and git installed. Make sure that your pip, setuptools, and wheel are up to date. When using pip it is generally recommended to install packages in a virtual environment to avoid changes to the system.