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Record W4412124549 · doi:10.1115/1.4069132

Reconstruction and Reduction of Realistic Manufacturing Error Field for Uncertainty Quantification of Transonic Axial Compressor Rotor

2025· article· en· W4412124549 on OpenAlexaff
Yaping Ju, Zhen Li, Xiawen Zhang, Yiming Liu, Chuhua Zhang

Bibliographic record

VenueJournal of Turbomachinery · 2025
Typearticle
Languageen
FieldEngineering
TopicManufacturing Process and Optimization
Canadian institutionsTrinity College
FundersNational Science and Technology Major ProjectNational Natural Science Foundation of China
KeywordsTransonicRotor (electric)Gas compressorReduction (mathematics)Field (mathematics)Axial compressorComputer scienceAerospace engineeringEngineeringMechanical engineeringMathematicsAerodynamicsGeometry

Abstract

fetched live from OpenAlex

Abstract Turbo compressors are inevitably subject to geometric and operational uncertainties that could induce performance degradations. This vulnerability is particularly pronounced in transonic compressor rotors due to the presence of sharp shock waves, which are highly susceptible to uncertainties. While the importance of uncertainty quantification (UQ) of compressors during the design phase has received growing recognition, the existing methodologies still face a grand challenge in modeling the geometric uncertainties related to manufacturing error fields. To address this challenge, we first propose an accurate geometric reconstruction method of realistic manufacturing error fields, in which kernel density estimation and correlation constraint sampling are combined to reconstruct manufacturing error fields with arbitrary probability distributions and geometric correlations. Then, a bilayer and bidirection dimension reduction method is proposed to treat the reconstructed model for reduced input uncertainties. The proposed methods are verified and validated by multipoint UQ of the well-known axial compressor rotor, i.e., NASA Rotor 37, under multisource uncertainties from blade manufacturing error fields as well as the total pressure, total temperature, and turbulence intensity of the incoming flow. From the statistics of 126 high-quality blades, each with 600 measurement points, it is confirmed that a large portion obey arbitrary probabilistic distributions rather than Gaussian distributions, and strong spatial correlations exist across the blade manufacturing error field. Both characteristics can be accurately reconstructed through the combination of kernel density estimation and correlation constraint sampling methods. Moreover, the bilayer and bidirection dimension reduction method is capable of reducing the dimensionality of manufacturing error field to 2–17 for Rotor 37, depending on the working points and performance parameters. The UQ results of Rotor 37 indicate that the geometric and operational uncertainties are mainly responsible for the mean offset and scatter of rotor performance variations, respectively. The geometric uncertainties due to manufacturing errors exert a negative impact on rotor performance, especially at near-stall point, manifested by increased suction-surface separation flow losses due to the forward shift of the shock wave. The proposed method in this work is quite generic and can be used in UQ and robust aerodynamic design optimization of turbomachinery components.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

How this classification was reachedexpand

Full frame distilled prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.

metaresearch head score (Codex)0.000
metaresearch head score (Gemma)0.000
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: none
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.674
Threshold uncertainty score0.308

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0000.000
Research integrity0.0000.000
Insufficient payload (model declined to judge)0.0000.000

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.012
GPT teacher head0.253
Teacher spread0.240 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it

Classification

machine, unvalidated

Machine predicted; a candidate call from one teacher head, not a consensus.

The models applied no category: nothing in the taxonomy fit this work.
Study designSimulation or modeling
Domainnot available
GenreEmpirical

How this classification was reached, model by model and score by score, is at the end of the page under "How this classification was reached".

Quick stats

Citations2
Published2025
Admission routes1
Has abstractyes

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