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Record W3035401587 · doi:10.2514/6.2020-2763

Effect of Leading-Edge Tubercles on Rotor Blades

2020· article· en· W3035401587 on OpenAlexaff
Robert R. Colpitts, Ruben E. Perez, Peter Jansen

Bibliographic record

VenueAIAA AVIATION 2020 FORUM · 2020
Typearticle
Languageen
FieldEngineering
TopicComputational Fluid Dynamics and Aerodynamics
Canadian institutionsRoyal Military College of Canada
Fundersnot available
KeywordsStall (fluid mechanics)Mach numberLeading edgeDragAirfoilTransonicPhysicsTrailing edgeAerodynamicsMechanics

Abstract

fetched live from OpenAlex

Current rotor blade designs are limited by retreating blade stall, influenced by local airfoil stall performance in root regions, as well as compressible flow effects and drag divergence of the advancing blade in the tip regions. The application of leading edge tubercles to lifting surfaces have shown to improve post-stall performance in the subsonic regime, and to delay shock-wave formation and improve drag divergence Mach numbers in the transonic regime. This paper explores the effects of leading edge tubercles applied to a canonical rotor. Various tubercle configurations were analyzed using computational fluid dynamic simulations using Euler and RANS equations. Improvements in Figure of Merit of 9.5% were found over the baseline rotor for specific tubercle configurations when operating at a pitch angle of 2 degrees and tip Mach number of 0.794. An increase in thrust coefficients and reduction in power coefficients over the baseline rotor were both attributed to alteration of flow behaviour in different regions of the rotor due to the presence of leading edge tubercles.

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)0.000
metaresearch head score (Gemma)0.001
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: none
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.001
Threshold uncertainty score0.004

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0000.001
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0010.000
Open science0.0000.001
Research integrity0.0000.000
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 head0.004
GPT teacher head0.211
Teacher spread0.207 · 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
Published2020
Admission routes1
Has abstractyes

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Same venueAIAA AVIATION 2020 FORUMSame topicComputational Fluid Dynamics and AerodynamicsFrench-language works237,207