MétaCan
Menu
Back to cohort
Record W2323208241 · doi:10.2514/6.2005-1892

Optimization of Aircraft Aeroelastic Response Using Level Set Methods

2005· article· en· W2323208241 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

Venue46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference · 2005
Typearticle
Languageen
FieldEngineering
TopicTopology Optimization in Engineering
Canadian institutionsUniversity of Victoria
FundersEuropean Social FundFundação para a Ciência e a Tecnologia
KeywordsAirfoilAeroelasticityAileronTopology optimizationActuatorCamber (aerodynamics)Computer scienceCompliant mechanismControl theory (sociology)Mathematical optimizationEngineeringWingAerodynamicsTopology (electrical circuits)Structural engineeringMathematicsAerospace engineering

Abstract

fetched live from OpenAlex

In this paper, we propose a new approach to the optimization of aircraft aeroelastic response that greatly reduces the number of design variables, thus enhancing the performance of multidisciplinary design tools. The current method is an extension of the Level Set Methods, which represent an interface as the zero level set of a function. According to the proposed formulation, the Fourier coefficients of the level set function are the design variables assigned to describe the interface. Two structural topology optimization examples and two applications to aircraft structures are presented. The first two examples deal with the optimal configuration of short and long cantilevered beams for maximum stiffness. In the first application, a system of actuators provides morphing capability to an airfoil by operating on its camber to increase lift. The problem consists in determining the airfoil profile that minimizes the power consumption while improving the airfoil effectiveness. In the second application, the aileron reversal speed is maximized by applying reinforcements to the upper skin of a wing torsion box. These four problems demonstrate that the proposed methodology is able to modify the topology of the interface while using a reduced number of design variables. Other advantages of this methodology include the partial avoidance of local non-global minima, by providing a mechanism for nucleation of new holes, and avoidance of checkerboard-like designs and sucessive remeshing.

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 categoriesMeta-epidemiology (narrow)
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: Simulation or modeling
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.142
Threshold uncertainty score0.999

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0010.001
Meta-epidemiology (broad)0.0010.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0010.000
Research integrity0.0010.000
Insufficient payload (model declined to judge)0.0010.000

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 head0.025
GPT teacher head0.288
Teacher spread0.263 · 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