Alternatives and similar repositories for LoadsKernel

Users that are interested in LoadsKernel are comparing it to the libraries listed below

• bennames / AeroComBAT-Project
  Aeroelastic Composite Beam Analysis Tool
  ☆19Updated 8 years ago
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆109Updated last month
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆49Updated 3 years ago
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆227Updated last week
• vsdsantos / nastran-aeroelasticity
  Some usefull routines for aeroelastic analysis with NASTRAN.
  ☆19Updated 3 years ago
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆116Updated this week
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆34Updated this week
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆126Updated last month
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆70Updated 2 years ago
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆160Updated 3 months ago
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆69Updated last week
• mdolab / openconcept
  OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
  ☆46Updated last month
• Mikekiely / wuFoil
  An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil
  ☆36Updated 2 months ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆103Updated 4 years ago
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆136Updated this week
• leal26 / AeroPy
  Python interface for XFOIL. The objective of this library is to be able to be able to call XFOIL from Python iteratively for any simulati…
  ☆73Updated 4 years ago
• NAnand-TUD / parablade
  A python based blade parametrization tool
  ☆63Updated last year
• seyk86 / dAEDalusNXT
  Aeroelastic Aircraft Design and Simulation Tool
  ☆29Updated 7 years ago
• VahanaOpenSource / vtol_sizing
  conceptual design of vtol platforms
  ☆16Updated 6 years ago
• mdolab / CMPLXFOIL
  ☆39Updated 5 months ago
• mid2SUPAERO / aerostructures
  Mapping, Radial Basis Function, RBF, FSI
  ☆12Updated 5 years ago
• rafaelpsilva07 / composipy
  composipy is a python library to calculate composite plates using the classical laminate theory. This library is designed to be simple, u…
  ☆40Updated 10 months ago
• The-Fonz / xfoil-optimization-toolbox
  The Python XFOIL optimization toolbox can be used to optimize airfoils for a specific operating range, and might be useful to you for its…
  ☆48Updated 8 years ago
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆17Updated 4 years ago
• marilib / MARILib
  Multidisciplinary Airplane Research Integrated Library
  ☆11Updated 5 years ago
• jte0419 / Panel_Methods
  Source and vortex panel method codes referenced in my YouTube videos.
  ☆101Updated 4 years ago
• OpenMDAO / Aviary
  NASA's aircraft analysis, design, and optimization tool
  ☆213Updated this week
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆36Updated 2 years ago
• usuaero / MachLine
  A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
  ☆45Updated 6 months ago
• swayli94 / cst-modeling3d
  Surface and foil modeling via CST method
  ☆25Updated 7 months ago