jxz21004

jxz21004's Stars

• bburke38/aob_funtofem

  Repository for Aeroelastic Optimization Benchmark implementation in FUNtoFEM.

  Language:Python2

• peterdsharpe/NeuralFoil

  NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.

  Language:Python18623

• cvxpy/cvxpy

  A Python-embedded modeling language for convex optimization problems.

  Language:C++5.7k1.1k

• ACea15/FENIAXexamples

  Examples for FENIAX codebase

  Language:Python21

• ACea15/FENIAX

  Language:Python146

• gaogaotiantian/coredumpy

  coredumpy saves your crash site for post-mortem debugging

  Language:Python51513

• AeroMAPS/AeroMAPS

  AeroMAPS: Multidisciplinary Assessment of Prospective Scenarios for air transport

  Language:Python202

• OpenVSP/OpenVSP

  A parametric aircraft geometry tool

  Language:C603307

• smdogroup/eigd

  Tools for eigenvector derivatives

  Language:Python63

• nasa/UQPCE

  Uncertainty Quantification using Polynomial Chaos Expansion (UQPCE) is an open source, python based research code for use in parametric, non-deterministic computational studies. UQPCE utilizes a non-intrusive polynomial chaos expansion surrogate modeling technique to efficiently estimate uncertainties for computational analyses. The software allows the user to perform an automated uncertainty analysis for any given computational code without requiring modification to the source. UQPCE estimates sensitivities, confidence intervals, and other model statistics, which can be useful in the conceptual design and analysis of flight vehicles. This software was developed for the Aeronautics Systems Analysis Branch (ASAB) within the Systems Analysis and Concepts Directorate (SACD) at NASA Langley Research Center to study potential impacts of uncertainties on the prediction of ground noise generated from commercial supersonic aircraft concepts.

  Language:Python4015

• deepseek-ai/DeepSeek-R1

  87.6k11.3k

• MDOBenchmarks/MDOAeroelasticBenchmark

  Aeroelastic Benchmark Problem

  Language:Python52

• OpenMDAO/POEMs

  Proposals for OpenMDAO Enhancements

  Language:HTML1529

• deepseek-ai/DeepSeek-V3

  Language:Python93.9k15.2k

• mdolab/AerostructuralOptBenchmark

  Language:Python124

• OpenMDAO/Aviary

  NASA's aircraft analysis, design, and optimization tool

  Language:Python17782

• A-CGray/FEMpy

  FEMpy is my attempt to implement a basic object-oriented finite element method in python that's as fast and flexible as possible.

  Language:Python62

• mdolab/aeroprop

  Language:Python61

• mdolab/dafoam

  DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization

  Language:C24894

• OpenMDAO/mphys

  Multiphysics with OpenMDAO

  Language:Python9837

• smdogroup/funtofem

  Adaptable framework for aerothermoelastic analysis and adjoint-based gradient evaluation

  Language:Python3025

• pygpc-polynomial-chaos/pygpc

  A Sensitivity and uncertainty analysis toolbox for Python based on the generalized polynomial chaos method

  Language:Jupyter Notebook8025

• smdogroup/tacs

  Finite-element library for analysis and adjoint-based gradient evaluation

  Language:C++11575

• OpenMDAO/OpenMDAO

  OpenMDAO repository.

  Language:Python596263