Skip to main content
This course introduces parametric turbomachinery design using signed distance functions in nTop. By building a micro turbojet, you will learn to create robust, reusable workflows for impellers, combustion chambers, and blisks. We focus on high-fidelity geometric construction and assembly, providing a foundation for integration with performance analysis and multidisciplinary design optimization.
Transparent view of turbine engine core: compressor, combustor, and turbine

Overview of Micro Turbojet Design

Parametric Impeller

Combustion Chamber

Parametric Bladed Disk

Parametric Housing and Component Placement