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FENIAX
Full aircraft trim + dynamic loads
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ACea15/FENIAX
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Getting started
Examples
Theoretical background
Architecture
Code base
FENIAX
ACea15/FENIAX
Home
Getting started
Examples
Examples
Summary
Sail Plane static response
Wing nonlinear dynamics
Free flying shell structure
Full aircraft (clamped) gust verification
Full aircraft trim + dynamic loads
Theoretical background
Theoretical background
Intrinsic modal description
Architecture
Architecture
JAX
UML description
Program inputs
Code base
Code base
Inputs
Modes
Nonlinear couplings
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