OpenConcept
Tutorials
Minimal Example
Using the Integrator
Turboprop Model and Mission Analysis
More Examples
Features
Aerodynamics
Atmospherics
Costs
Energy Storage
Geometry
Mission
Propulsion
Stability
Thermal
Weights
Utilities
Other Useful Docs
Source Docs
openconcept.aerodynamics
openconcept.aerodynamics.openaerostruct
openconcept.atmospherics
openconcept.costs
openconcept.energy_storage
openconcept.energy_storage.hydrogen
openconcept.geometry
openconcept.mission
openconcept.propulsion
openconcept.propulsion.systems
openconcept.stability
openconcept.thermal
openconcept.utilities
openconcept.utilities.math
openconcept.weights
weights_BWB.py
weights_jet_transport.py
weights_turboprop.py
weights_twin_hybrid.py
Development Roadmap
Publications
OpenConcept
Source Docs
openconcept.weights
weights_twin_hybrid.py
View page source
weights_twin_hybrid.py