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Record W4416405391 · doi:10.1016/j.rineng.2025.108244

Assessment of the sensitivity of high-lift airfoil performance to flap gap and overlap

2025· article· en· W4416405391 on OpenAlexaff
D. J. Cerantola, Mohsen Ferchichi, Mohamed Sadok Guellouz

Bibliographic record

VenueResults in Engineering · 2025
Typearticle
Languageen
FieldEngineering
TopicBiomimetic flight and propulsion mechanisms
Canadian institutionsRoyal Military College of CanadaQueen's University
Fundersnot available
KeywordsAirfoilComputational fluid dynamicsReynolds-averaged Navier–Stokes equationsTurbulenceLift (data mining)Parametric statisticsWakeAngle of attack

Abstract

fetched live from OpenAlex

• A detailed parametric study investigates the effects of flap gap and overlap on high-lift airfoil performance. • CFD simulations using the SST turbulence model show good agreement with experimental PIV data. • Increasing flap gap and overlap leads to reduced lift and higher drag, with overlap having the greater impact. • Lift enhancement is strongly correlated with suction peak pressure, slot jet velocity, and slot length. • Slot flow momentum improves wake mixing but increases flap recirculation due to slot geometry. A numerical investigation and experimental validation of the flow dynamics of a high-lift airfoil were performed to develop a numerical model for an extended parametric study. Although Computational Fluid Dynamics (CFD) has become a valuable design tool for the aerospace community in the quest for improved wing design, several challenges remain in accurately predicting the flow field of a stalled multi-element airfoil owing to inadequate modelling choices and insufficient grid resolution. In this study, the commercial solver ANSYS Fluent was used to conduct a parametric study by varying the flap gap and overlap of a Fowler flap with a flap deflection of 40° and an angle of attack of 0° The results showed that the velocity, vorticity, and turbulence intensity fields predicted by the 2D steady-state RANS solutions using Menter's SST turbulence model were in good agreement with the experimental PIV data. The parametric study revealed that the wing performance decreased as the slot length increased, which was attributed to the aggravation of flap stall. An empirical correlation relating lift performance to flow and geometric parameters was developed, providing a simplified predictive framework for the considered angle of attack and flap deflection.

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: Simulation or modeling
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.162
Threshold uncertainty score0.349

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 head0.006
GPT teacher head0.215
Teacher spread0.209 · 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

Citations1
Published2025
Admission routes1
Has abstractyes

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