Preview
Web-Based Design Interface
Create a project, enter design requirements, and get instant results — meridional view, blade profiles, geometry parameters, performance, and flow states.
BraytonWorks is an AI-powered turbomachinery design platform specialized for gas turbine engines.
From thermodynamic cycle analysis to component-level meanline design, blade geometry generation,
and CFD-ready output — all in one integrated web application.
An end-to-end gas turbine design platform that connects every stage of the process.
Real-time matching between thermodynamic cycle analysis and individual component performance. Change a compressor PR and see the impact on turbine inlet temperature instantly.
Design all gas turbine components simultaneously — compressor, combustor, turbine — with automatic performance matching across the engine. No more isolated spreadsheets.
AI agents assist throughout the entire design process: parameter recommendations, result interpretation, design trade-off analysis, and knowledge-base verified guidance.
Available now and coming soon.
Axial compressor multi-stage sizing available now. Centrifugal compressor, axial turbine, and radial turbine sizing coming soon.
4-plane Mach-based solver with Koch-Smith loss model. Design-point analysis with choke detection. Off-design and performance maps coming soon.
Gas turbine thermodynamic cycle analysis for various engine configurations: turbojet, turbofan, turboshaft, turboprop, and industrial gas turbines. Coming soon.
Parametric 3D blade generation, throughflow analysis, blade-to-blade (B2B), and 3D CFD integration. From meanline to high-fidelity validation. Coming soon.
Meridional view, blade profile cascade (HMT overlay), geometry parameters, performance tables, and full flow states — all interactive in the browser.
AI agents at every design step: sizing recommendations, result interpretation, trade-off analysis, and knowledge-base verified guidance. Coming soon.
From engine-level cycle to component-level blade geometry — all connected.
Create a project, enter design requirements, and get instant results — meridional view, blade profiles, geometry parameters, performance, and flow states.
Current progress and future plans.
4-plane Mach solver, Koch-Smith loss model, multi-stage axial compressor sizing with RE, web UI with 5 design views.
React + FastAPI, meridional/blade profile/geometry/performance/flow views, machine.json SSOT, Fly.io deployment.
Extend component sizing and meanline analysis to all major turbomachinery types.
Thermodynamic cycle for turbojet, turbofan, turboshaft, turboprop, industrial GT. Real-time cycle-component matching.
Real-time performance matching across engine. Change any component parameter, see system-level impact immediately.
Parametric 3D blade, throughflow (S2), blade-to-blade (S1), 3D CFD. Progressive fidelity from meanline to high-resolution.
AI agents at every design step: sizing, analysis, optimization, CFD setup. Natural language control and knowledge-base guidance.
BraytonWorks is free to use during the preview period.
Create your first axial compressor design in seconds.
Gas turbine OEMs, MRO companies, and turbomachinery manufacturers — provide real-world design requirements and validation data.
Engineers and developers in turbomachinery aerodynamics, CFD, AI/ML, and web development.