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Record W2524386787 · doi:10.11159/icmie16.129

Fluid-Structure Coupled Analysis of a Fabric-Covered Airfoil

2016· article· en· W2524386787 on OpenAlexvenueno aff
Jae-Sunbe Bae, Soo‐Yong Lee, Hark-Bong Kim, Jungsun Park

Bibliographic record

VenueProceedings of the World Congress on Mechanical, Chemical, and Material Engineering · 2016
Typearticle
Languageen
FieldEngineering
TopicWind Energy Research and Development
Canadian institutionsnot available
FundersKorea Institute of Energy Technology Evaluation and PlanningKorea Evaluation Institute of Industrial TechnologyMinistry of Trade, Industry and Energy
KeywordsAirfoilComputer scienceMarine engineeringAerospace engineeringEngineering

Abstract

fetched live from OpenAlex

Extended Abstract Wind turbines (WTs) rapidly become bigger than bigger but conventional WT blade designs have still used fiberglass. Though fiberglass is cheaper than advanced materials like carbon composites it is heavy and its manufacturing process is extremely hands-on time intensive. This conventional WT blade design may not be good for the development of advanced WT blades. A new approach to design, manufacture, and install WT blades will be necessary in the near future. The use of architectural fabrics could change the conventional design of the WT blades [1] and could reduce the manufacturing costs of very large blade manufacturing 25% to 40%. This fabric-covered wind turbine blade is composed of spars, ribs and covering fabrics similar to the truss structure of the aircraft wings. In this concept, the front and rear spars sustain all of the loads like bending moments of a wing. The fabric-skin is mainly subjected to torque and keeps the airfoil shape. This fabric skin acts like a membrane and is deformed by the pressure acting on it. If it deforms the pressure distribution acting on it is also changed and consequently the fabric skin deforms again. Finally, due to the fabric skin deformation, the aerodynamic characteristics of the blade and wing are changed and the aeroelastic characteristics of the fabric skin should be investigated. In the present study, the aerodynamic deformations and aeroelastic characteristics of the fabric skin are studied. The membrane analysis of the fabric skin is performed for its structural modelling and the CFD (computational fluid dynamics) analysis of the airfoil section is performed by using ANSYS. The present membrane analysis results and CFD results are verified by comparing the reference results. Finally, the fluid-structure coupled analsys of the fabric skin are performed and its aerodynamic deformations, deformed pressure distributions, and aeroelastic characteristics are investigated.

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: Bench or experimental · Consensus signal: Bench or experimental
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.010
Threshold uncertainty score0.596

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 head0.004
GPT teacher head0.183
Teacher spread0.179 · 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 designBench or experimental
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

Citations0
Published2016
Admission routes1
Has abstractyes

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