HENSTRUCT · Aeronautical Engineering

Thermo-Structural Analysis in HENSTRUCT

αΔT thermal stress and graph-Laplace heat → expansion → stress paths for propulsion-heated and high-speed skins.

Hendoi TechnologiesRelated: HENSTRUCT

Propulsion-heated skins and high-speed vehicles add temperature fields to structural decisions. HENSTRUCT supports αΔT thermal stress and thermo-structural paths from heat to expansion to stress.

Start with the temperature story

Import or prescribe nodal temperatures. Uncertain thermal BCs dominate MoS more often than mesh density.

Couple carefully

Use the graph-Laplace heat path when you need a consistent temperature field before expansion. Document material α(T) assumptions.

Related suite products

External aeroheating contexts may begin in HENFLOW; structural response lands in HENSTRUCT after HENMESH prep.

How HENSTRUCT helps you act

Treat thermo-structural MoS as a named load family in design review. License via support@hendoi.com.