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Record W4317633779 · doi:10.2514/6.2023-1619

A Deep-Learning Surrogate Model Approach for Optimization of Morphing Airfoils

2023· article· en· W4317633779 on OpenAlex

Why this work is in the frame

A frame that forgets how it found something cannot be audited. These are the routes that admitted this work.

affAt least one author lists a Canadian institution in the pinned OpenAlex snapshot.

Bibliographic record

VenueAIAA SCITECH 2023 Forum · 2023
Typearticle
Languageen
FieldPhysics and Astronomy
TopicModel Reduction and Neural Networks
Canadian institutionsUniversity of TorontoFields Institute for Research in Mathematical Sciences
Fundersnot available
KeywordsMorphingComputer scienceAirfoilSurrogate modelDeep learningArtificial intelligenceMachine learningAerospace engineeringEngineering

Abstract

fetched live from OpenAlex

View Video Presentation: https://doi.org/10.2514/6.2023-1619.vid Analyzing and optimizing the aerodynamic performance of a morphing airfoil concept typically requires the numerical solution of many complex, computationally expensive fluid-structure interaction (FSI) problems. This approach becomes intractable against current developments in intelligent, programmable materials and additive manufacturing techniques, which drastically increase the design space and open novel opportunities for passively and actively morphing wings. To fully exploit these capabilities, a new paradigm for analyzing and optimizing aeroelastic structures in high-dimensional parameter spaces is required. This work presents an efficient numerical design approach for elastically morphing structures in aerodynamic flows. Our approach centers on using deep neural network surrogate models to predict the aerodynamic loading as a function of a given shape. The models are trained through a set of flow simulations around rigid stationary bodies randomly sampled from a parametrized design space of the shapes. Once trained, the surrogate model can be used to evaluate the aerodynamic performance of any structural design without the need for further costly flow or FSI simulations. Consequently, this approach can analyze and optimize airfoils within a higher-dimensional structure and structure-actuator problems than currently possible. Though the approach is general, we focus here on establishing a proof-of-concept of this idea for a 2D multi-hinged airfoil at a steady-state condition. The specific contributions are validating the surrogate model, estimating the cost benefits of this approach, and providing first insights into the approach's capabilities. A practical optimization of a 2D morphing airfoil in steady flows demonstrates that training and using the surrogate model reduces the number of required flow solutions by several orders of magnitude compared with a fully coupled FSI approach.

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.

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: Simulation or modeling
GenreCandidate signal: Methods · Consensus signal: none
Teacher disagreement score0.957
Threshold uncertainty score0.534

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.001
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 head0.023
GPT teacher head0.259
Teacher spread0.236 · 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