Vertical 4 completes the current set: transonic compressor prediction. ⚙️
Transonic compressor blades operate where small geometric changes produce large aerodynamic consequences — shock position, loss, and stall margin all shift together. Exploring that design space properly requires far more analyses than a conventional CFD budget allows.
The model is trained on NASA Rotor 37, the transonic compressor rotor that has served as a validation benchmark for turbomachinery CFD for decades — which means our results can be compared against a case the whole field already knows. It predicts the flow field around the blade at a single operating point for now, with extension to full performance maps to follow.
With four verticals online — transformers, motorbike aerodynamics, ship hulls and now compressors — the Spaider-AI platform covers conjugate heat transfer, external aerodynamics, multiphase flow and turbomachinery. Each one is a different physics problem, solved by the same underlying approach.
👉 See the compressor vertical — or book a conversation with us.