Native desktop · aeronautical / aerospace structural FEA
HENSTRUCT
HENSTRUCT is Hendoi’s structural desk for aeronautical and aerospace programmes: linear through nonlinear static, modal and vibration paths, buckling, composites, fatigue, thermo-structural coupling, aeroelasticity/flutter/gust, margins, and V&V. Geometry from HFOIL; meshes from HENMESH; aero loads optionally from HENFLOW.
Keep structural analysis inside the aerospace domain. HENSTRUCT specialises in flight programmes so load cases, composites, flutter, and margins speak MoS and FAR/CS language — not generic CAE menus.
Signature capabilities
HENSTRUCT is scoped to aeronautical and aerospace programmes: airframes, UAV/eVTOL structures, composites, aeroelastic coupling, rotor and landing-gear events. Not automotive crash, civil structures, or general mechanical CAE.
Project manager, materials, aerospace load cases, solver families from linear static through flutter, post-processing, margins of safety, PDF reports, optimisation, validation benchmarks, and HPC foundations — organised as a structures desk.
Prepare geometry in HFOIL (CAD), mesh and quality-gate structural volumes in HENMESH, then solve strength, dynamics, and margins in HENSTRUCT. Couple pressure loads from HENFLOW when aeroelasticity or gust needs them.
Linear/nonlinear static, modal, harmonic FRF, random vibration, response spectrum, transient, buckling/Riks, composites, fatigue/fracture, thermo-structural, aeroelastic/flutter/gust, rotor, landing gear, joints, MoS, load cases, optimisation, V&V, and HPC.
Named thrust/fuel/payload combinations, FAR/CS-style factors, UnifyMargins API, and review-ready MoS outputs so strength decisions survive design reviews.
HENSTRUCT does not replace HFOIL or HENMESH. It owns the structural solve, post, margins, and reports once the mesh and materials story is ready.
Hendoi product chain
Aeronautical CAD and geometry shortlists. Open HFOIL →
Phase 6 prep, HEN-AI, quality gates, suite export. Open HENMESH →
Aerospace CFD campaigns when you need pressures and forces. Open HENFLOW →
Aerospace structural FEA — strength, dynamics, MoS — this product.
Full feature catalogue
Organised for flight structures — with Production / Foundation / Roadmap maturity called out in the desktop capability map.
Typical workflow
Bring a quality-gated structural mesh from HENMESH (or an approved FEM bridge). Confirm units, element types, and material regions.
Metals, composites (CLT stacks), connectors, and temperature-dependent properties for thermo-structural cases.
Named manoeuvre, gust, thrust, fuel, and payload combinations — with FAR/CS-style factors where your programme requires them.
Dispatch linear/nonlinear static, modal, harmonic, buckling, aeroelastic, or specialty paths. Monitor residuals and energy checks.
Inspect stress/strain/modes; run UnifyMargins; export PDF strength packages for design review.
Size/topology or GA/PSO paths under hard constraints; run V&V benchmarks before trusting production MoS.
Who it serves
HENSTRUCT is Hendoi’s native desktop structural FEA workbench for aeronautical and aerospace programmes: strength, dynamics, buckling, composites, fatigue, thermo-structural coupling, aeroelasticity, margins, and validation — not a general industrial FEA suite.
Learn
Import a HENMESH structural mesh, assign materials and aerospace load cases, run a monitored static solve, and review margins — native desktop aerospace FEA.
Read more →HENSTRUCTDisplacement, stress, strain, reactions, and energy-balance checks for airframe strength cases — with FAR/CS-minded load booking.
Read more →HENSTRUCTFrequencies, mode shapes, participation factors, and complex FRF paths for vibration and forced-response desks.
Read more →HENSTRUCTLinear eigen buckling plus spherical Riks arc-length continuation past λ_cr for thin aerospace structures.
Read more →HENSTRUCTCLT ABD stacks with Tsai–Hill/Wu, Hashin, and Max Stress/Strain criteria for laminated airframe components.
Read more →HENSTRUCTGoodman/Basquin, ASTM E1049 rainflow Miner, LCF, and Paris DT fracture proxies for durability programmes.
Read more →HENSTRUCTαΔT thermal stress and graph-Laplace heat → expansion → stress paths for propulsion-heated and high-speed skins.
Read more →HENSTRUCTStatic aeroelastic redistribution, modal flutter with Ka/Ca, and Pratt V–n / 1-cosine gust transients — optionally seeded by HENFLOW pressures.
Read more →HENSTRUCTNamed thrust/fuel/payload combinations, FAR/CS-style factors, UnifyMargins API, and review-ready MoS packages.
Read more →HENSTRUCTA clear decision guide: aeronautical CAD vs mesh prep vs aerospace CFD vs aerospace structural FEA — and when to call custom solver services.
Read more →HENSTRUCT
Straight answers about aerospace-only FEA scope, CAD/mesh handoff, margins, and licensing.
HENSTRUCT is Hendoi’s native desktop structural FEA product for aeronautical and aerospace analysis only — linear through nonlinear static, dynamics, buckling, composites, fatigue/fracture, thermo-structural, aeroelasticity/flutter/gust, margins, optimisation, validation, and HPC foundations.
No. It deliberately focuses on aerospace structures so load cases, margins, composites, flutter, and gust speak flight-programme language — not generic mechanical CAE menus.
No. It is solver-only. Prepare geometry in HFOIL and structural meshes in HENMESH, then solve and report in HENSTRUCT.
Typical chain: geometry in HFOIL → structural mesh in HENMESH → solve in HENSTRUCT. When aeroelastic or gust cases need pressure fields, couple loads from HENFLOW CFD campaigns.
Native desktop builds for Windows, Linux, and macOS (C++ / HendoiUI). Commercial, lab, and academy licensing is available worldwide via Contact.
Core static, modal, buckling, composites, fatigue, margins, and load-case paths are productised for aerospace desks. Specialty flutter, HPC MPI, and some optimisation paths carry foundation/roadmap maturity — ask for the current capability map on a demo call.