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Record W2026024375 · doi:10.5589/q05-007

Investigation of an Asymmetrical Shock-Wave Boundary-Layer Interaction in a Supersonic Planar Nozzle

2005· article· en· W2026024375 on OpenAlexvenueno aff
Alexis Bourgoing, R. Benay

Bibliographic record

VenueCanadian aeronautics and space journal · 2005
Typearticle
Languageen
FieldEngineering
TopicAerodynamics and Acoustics in Jet Flows
Canadian institutionsnot available
Fundersnot available
KeywordsSupersonic speedBoundary layerTurbulenceNozzleMechanicsTransonicShock (circulatory)PhysicsReynolds-averaged Navier–Stokes equationsShock waveMach numberWind tunnelAerospace engineeringAerodynamicsEngineering

Abstract

fetched live from OpenAlex

When thrust nozzles are designed for high-altitude flight regimes, the propulsive jet is no longer adapted for operation at ground level and at low altitude. Thus, the nozzle operates in over-expanded regime. Unsteadiness due to the boundary layer/shock interactions in the divergent part of the nozzle can produce non-symmetric side loads that can damage the structure. The need for a complete understanding of this phenomenon and the validation of numerical methods and turbulence models able to predict this phenomenon has motivated a basic experiment aimed at producing an exhaustive set of experimental data. The test configuration made up of a rectangular nozzle and set up in a supersonic wind tunnel has allowed us to obtain a non-symmetric interaction whose unsteady aspects have been analyzed. This program was completed by numerical simulations of the flow in its mid-longitudinal symmetry plane. The goal was to test the capabilities of RANS (Reynolds Average Navier–Stokes) calculations in predicting the mean interacting flow through the use of three two-equation turbulence models. Two models, recently tested in the case of transonic and supersonic separations, compared with the Jones–Launder model, have given close results. Experimental and theoretical data have constituted the matter for a general discussion of the validation of turbulence models in channel flows where acoustic disturbances appear.

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: Bench or experimental · Consensus signal: Bench or experimental
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.002
Threshold uncertainty score0.005

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0000.001
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0010.000
Bibliometrics0.0000.000
Science and technology studies0.0010.001
Scholarly communication0.0010.000
Open science0.0000.001
Research integrity0.0010.001
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 head0.018
GPT teacher head0.217
Teacher spread0.198 · 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 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

Citations2
Published2005
Admission routes1
Has abstractyes

Explore more

Same venueCanadian aeronautics and space journalSame topicAerodynamics and Acoustics in Jet FlowsFrench-language works237,207