A Multi-Dimensional Machine Learning Framework for Superior Propeller Design Choices

In this study, PropAI is presented, which is a scalable, multi-dimensional surrogate modelling framework for propeller performance prediction that compiles a large 5D baseline database and couples it to a KD-tree Gaussian radial-basis-function (RBF) interpolator. A full-factorial sweep over five design parameters (rotational speed, freestream velocity, blade pitch, diameter, and number of blades) yields 88,540 operating points evaluated via low-fidelity BEMT in QBlade. The trained surrogate reproduces these data with near-machine precision (global RMSE = 6.2e-4, MAE = 1.0e-5, R2 = 1.000), and parity plots of predicted vs true thrust and power lie essentially on the 45 deg line (1:1 line). Cross-validation of leave-one-out (LOO) errors confirms excellent generalisation, with both thrust and power below 0.6% of full-scale output. Integrated with an UNSGA‑III optimiser, the model performs multi-objective optimisation of thrust, power, and thrust-to-power ratio, producing Pareto fronts that reveal the trade-offs among these metrics. This lightweight, gradient-capable surrogate enables rapid design-space exploration (e.g. via 1D/2D response slices, pair-plots, parallel coordinates) and provides insight into parametric interactions.

Authors

Institutions

Publication Details

Published
2025-07-16
DOI
https://doi.org/10.2514/6.2025-3423
Citations
1
Primary Topic
Advanced Aircraft Design and Technologies
Type
article
Field-Weighted Citation Impact
1.11
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

A Multi-Dimensional Machine Learning Framework for Superior Propeller Design Choices

Shubham Shubham, Anupama Sharma
1 citations
Advanced Aircraft Design and Technologies
1.11
article

A Multi-Dimensional Machine Learning Framework for Superior Propeller Design Choices

Shubham Shubham, Anupama Sharma
article en
1 citations

Abstract

In this study, PropAI is presented, which is a scalable, multi-dimensional surrogate modelling framework for propeller performance prediction that compiles a large 5D baseline database and couples it to a KD-tree Gaussian radial-basis-function (RBF) interpolator. A full-factorial sweep over five design parameters (rotational speed, freestream velocity, blade pitch, diameter, and number of blades) yields 88,540 operating points evaluated via low-fidelity BEMT in QBlade. The trained surrogate reproduces these data with near-machine precision (global RMSE = 6.2e-4, MAE = 1.0e-5, R2 = 1.000), and parity plots of predicted vs true thrust and power lie essentially on the 45 deg line (1:1 line). Cross-validation of leave-one-out (LOO) errors confirms excellent generalisation, with both thrust and power below 0.6% of full-scale output. Integrated with an UNSGA‑III optimiser, the model performs multi-objective optimisation of thrust, power, and thrust-to-power ratio, producing Pareto fronts that reveal the trade-offs among these metrics. This lightweight, gradient-capable surrogate enables rapid design-space exploration (e.g. via 1D/2D response slices, pair-plots, parallel coordinates) and provides insight into parametric interactions.

Cranfield University (GB)
Affordable and clean energy
Openalex Percentile: Top 22%
Advanced Aircraft Design and Technologies
1.11
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.