NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
The Effect of Training Data on Predicting Turbulent Flow Through a Linear Cascade Using Physics-Informed Neural NetworksThis paper investigates the effect of training data on the accuracy of turbulent flow predictions in the wake region of a linear turbine cascade using physics-informed neural networks (PINNs). While it is well known that PINNs can solve the unclosed Reynolds-averaged Navier-Stokes (RANS) equations when sufficient training data are available, the specific characteristics of the data – such as the quantity and location– required for accurate predictions remain largely uncertain. To explore this, a PINN is constructed to solve the unclosed compressible RANS equations leveraging training data from a CFD solution of a turbine blade. The training data are then selectively sampled with future optical test campaigns in mind. This sampling includes varying the pitchwise surveys with evenly spaced training points, randomly sampled points, and CFD-guided sampling. For each case, the PINN is trained on data for the velocity components, temperature, pressure, and Reynolds stresses. Good agreement is seen between the PINNs-predicted quantities and the CFD solution, even in areas where the PINN wasn’t provided training data and excellent agreement in regions where data were provided. It’s shown that the PINN can provide acceptable solutions to the unclosed RANS equations when provided with roughly 100 data points downstream of the blade, and even better results when provided with roughly 200 points. This shows promise for future test campaigns which seek to combine AI-based tools with experimental techniques.
Document ID
20250006210
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Ezra O McNichols
(Glenn Research Center Cleveland, United States)
Jeffrey P Bons
(The Ohio State University Columbus, United States)
Date Acquired
June 13, 2025
Subject Category
Aerodynamics
Report/Patent Number
GT2025-153885
Meeting Information
Meeting: Turbomachinery Technical Conference & Exposition
Location: Memphis, TN
Country: US
Start Date: June 16, 2025
End Date: June 20, 2025
Sponsors: The American Society of Mechanical Engineers (ASME)
Funding Number(s)
WBS: 081876.02.03.50.19.02
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
cascade
turbine
aerodynamics
physics-informed neural networks
deep learning
Machine learning
No Preview Available