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Record W1997128974 · doi:10.2514/1.j052380

Subsonic Jet Noise Simulations Using Both Structured and Unstructured Grids

2014· article· en· W1997128974 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.
fundA Canadian funder is recorded on the work.

Bibliographic record

VenueAIAA Journal · 2014
Typearticle
Languageen
FieldEngineering
TopicAerodynamics and Acoustics in Jet Flows
Canadian institutionsUniversité de Sherbrooke
FundersCompute Canada
KeywordsJet noiseLarge eddy simulationJet (fluid)Computational aeroacousticsNozzleMach numberDiscontinuous Galerkin methodTurbulenceUnstructured gridNoise (video)GridDiscretizationContext (archaeology)Dissipative systemReynolds numberPhysicsTotal variation diminishingMechanicsComputer scienceAeroacousticsComputational fluid dynamicsFinite element methodGeometryAcousticsMathematicsMathematical analysisGeology

Abstract

fetched live from OpenAlex

For the last 10 years, large-eddy simulations have become a major tool for investigating jet noise sources because of their intrinsic ability to capture broadband turbulent features. However, many challenges still arise when dealing with complex geometries in terms of method accuracy and computational costs. Two different approaches to compute jet noise in an industrial context are here validated and compared. Both approaches are based on a hybrid methodology combining large-eddy simulation of jet flows for sources computations and Ffowcs Williams and Hawkings’s analogy for far-field noise prediction, but they differ on their grid topologies. The first approach uses classical block structured grids. The numerical scheme is a low-dispersive, low-dissipative finite-volume compact scheme. The second approach uses fully unstructured tetrahedral grids with a low-dispersive, low-dissipative Taylor–Galerkin finite-element scheme. Both approaches are used to compute a Mach 0.9 cold jet at the moderate Reynolds number without accounting for the nozzle geometry. Comparisons between simulations and experimental measurements highlight the need to correctly capture the initial turbulent development of the mixing layer at the nozzle exit. In the present simulations, because the nozzle geometry is not discretized, the turbulent transition is done by injecting perturbations as vortex-ring modes. Results obtained on this benchmark test case demonstrate the capability of both methods to correctly simulate and predict jet noise. The validation of the approach using fully tetrahedral grids provides a promising way to account for complex noise-reduction devices such as chevrons, realistic dual-stream nozzles, or lobed mixers.

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 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 score0.091
Threshold uncertainty score0.537

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 head0.007
GPT teacher head0.213
Teacher spread0.206 · 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