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Record W2328843689 · doi:10.2514/6.2010-1433

Higher Order Two Dimensional Aerodynamic Optimization Using Unstructured Grids and Adjoint Sensitivity Computations

2010· article· en· W2328843689 on OpenAlexafffund
Mohammad Y. Azab, Carl Ollivier‐Gooch

Bibliographic record

Venue48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition · 2010
Typearticle
Languageen
FieldEngineering
TopicComputational Fluid Dynamics and Aerodynamics
Canadian institutionsUniversity of British Columbia
FundersNatural Sciences and Engineering Research Council of Canada
KeywordsAerodynamicsSensitivity (control systems)ComputationUnstructured gridComputer scienceMathematical optimizationComputational scienceApplied mathematicsParallel computingComputational fluid dynamicsAlgorithmAerospace engineeringMathematicsElectronic engineeringEngineering

Abstract

fetched live from OpenAlex

*† We present early results from an aerodynamic optimization scheme based on a high-order accuracy finitevolume solver. The flow solution sensitivity is calculated using the adjoint approach; the higher order method is shown to be more accurate in calculating sensitivity values than traditional second order accurate computations, when each is compared to the finite difference sensitivity for a flow solver of the same order of accuracy. We take advantage of the exact Jacobian matrix to simplify this process. To avoid re-generating the grid around the airfoil for each optimization iteration, we instead deform the mesh when the geometry is change. We use the semi-torsional mesh movement scheme because of its simplicity and robustness. We use The Quasi-Newton optimization line search method with BFGS approximation of the Hessian matrix as an optimization scheme. We present two unconstrained optimization test cases: one with angle of attack as the sole design variable, and the other an inverse design shape optimization problem. Both the 2 nd and 4 th order schemes reach their corresponding optimal solutions with identical optimization convergence rates. The 2 nd and 4 th order schemes produces similar airfoil shapes for the inverse design test case in subsonic conditions.

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 machine prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. The Gemma side is a direct model label for every work in the frame, read from the title-only record. The Codex side is a classifier learned from the 10,348 direct Codex labels and calibrated to design-weighted sample rates; fields without enough sample support carry no Codex call. Candidate is the union of the two sides; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels.

metaresearch head score (Codex)0.001
metaresearch head score (Gemma)0.003
Version: metacan-v3-hybrid-931329e0061cValidation 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: Empirical · Consensus signal: none
Teacher disagreement score0.004
Threshold uncertainty score0.008

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0010.003
Meta-epidemiology (narrow)0.0010.000
Meta-epidemiology (broad)0.0010.001
Bibliometrics0.0000.000
Science and technology studies0.0000.001
Scholarly communication0.0010.001
Open science0.0010.001
Research integrity0.0010.001
Insufficient payload (model declined to judge)0.0020.000

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 head0.011
GPT teacher head0.247
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

Classification

machine, unvalidated

Machine predicted; a candidate call from one source (direct Gemma or distilled Codex), 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

Citations3
Published2010
Admission routes2
Has abstractyes

Explore more

Same venue48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace ExpositionSame topicComputational Fluid Dynamics and AerodynamicsFrench-language works237,207