MétaCan
Menu
Back to cohort
Record W4232555358 · doi:10.22215/etd/2017-12184

Investigating the Impact of Using CFD Generated Unsteady Mach Number Dynamic Stall Data for Numerical Rotor Analysis of Helicopter Forward Flight

2017· dissertation· en· W4232555358 on OpenAlexafffund
Dustin Jee

Bibliographic record

Venuenot available
Typedissertation
Languageen
FieldEngineering
TopicComputational Fluid Dynamics and Aerodynamics
Canadian institutionsCarleton University
FundersNatural Sciences and Engineering Research Council of CanadaGovernment of Ontario
KeywordsStall (fluid mechanics)FreestreamComputational fluid dynamicsAerodynamicsMach numberPitching momentAerospace engineeringHelicopter rotorComputer scienceEngineeringMechanicsRotor (electric)Angle of attackPhysicsMechanical engineeringTurbulenceReynolds number

Abstract

fetched live from OpenAlex

When the rotor blades are at a high advance ratio and/or a high thrust coefficient, the onset of dynamic stall makes accurate prediction of airloads on the rotor blades difficult.Comprehensive rotor analysis codes used in the industry rely on semi-empirical dynamic stall models to generate the aerodynamic coefficients of the blade sections undergoing dynamic stall.However, these models neglect the unsteady nature of the freestream seen by the blade sections compromising the accuracy of the analysis at high speed forward flight and high blade loading conditions.Thus, this thesis aims to investigate the impact of including the unsteady freestream effects in dynamic stall for the prediction of the airloads on the rotor blades.To study the impact of including the unsteady nature of the freestream in dynamic stall, Computational Fluid Dynamics (CFD) was used to generate the unsteady 2D dynamic stall aerodynamic data.The CFD data then served as inputs to the in-house rotor analysis code called Qoptr to generate blade airload results.The flight test data from a steady-level flight case (C T /σ = 0.129, µ = 0.24) from the UH-60A Airloads program was used for validation.The Qoptr blade airload results generated with the unsteady CFD dynamic stall data showed considerably better agreement with the flight test data than the results generated with semi-empirical dynamic stall models, especially in the sectional moment results.

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: Empirical
Teacher disagreement score0.003
Threshold uncertainty score0.007

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0010.003
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0010.001
Open science0.0000.000
Research integrity0.0010.000
Insufficient payload (model declined to judge)0.0010.001

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 head0.029
GPT teacher head0.345
Teacher spread0.316 · 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

Citations0
Published2017
Admission routes2
Has abstractyes

Explore more

Same topicComputational Fluid Dynamics and AerodynamicsFrench-language works237,207