MétaCan
Menu
Back to cohort
Record W2328108246 · doi:10.2514/6.2008-5272

Extending the Capabilities of a High-Speed Wind Tunnel to Secondary Flow Measurements in Transonic Linear Turbine Cascades

2008· article· en· W2328108246 on OpenAlexaff
Farzad Taremi, S. A. Sjolander, Hamza Abo El Ella

Bibliographic record

Venuenot available
Typearticle
Languageen
FieldEngineering
TopicTurbomachinery Performance and Optimization
Canadian institutionsCarleton University
Fundersnot available
KeywordsTransonicWind tunnelTurbineFlow (mathematics)Aerospace engineeringSubsonic and transonic wind tunnelMarine engineeringComputer scienceEngineeringPhysicsMechanicsAerodynamics

Abstract

fetched live from OpenAlex

Since its commissioning, the Carleton University High-Speed Wind Tunnel has been used extensively for midspan aerodynamic measurements in transonic axial turbine cascades. Recently, a requirement has arisen to obtain three-dimensional, endwall flow data in turbine cascades in this facility. Three dimensional loss measurements in high-speed turbomachinery cascades and rotating rigs have often been obtained using Kiel probes. These probes have the advantage of giving direct measurements of the total pressures, thus allowing losses to be obtained with minimal data reduction and without resort to complex probe calibrations. On the other hand, they cannot be used to obtain flow direction and local estimates of static pressure. As a result they do not permit other important information to be obtained, such as secondary kinetic energy, axial velocity and vorticity distributions. This limits the ability to gain physical insights into the flow behaviour. An alternative to Kiel probes is the multi-hole pressure probe. The present study was intended to develop the ability to obtain detailed three-dimensional flow field measurements in our facility using primarily a seven-hole pressure probe. The measurements are compared with the equivalent total pressure measurements obtained with a Kiel probe of similar spatial resolution. The uncertainty in losses introduced by the processing of multiple pressure-port measurements, and the use of complex probe calibration data, is weighed against the advantages of the more detailed flow field data that are obtained. The results from two linear turbine cascades with different Zweifel coefficients are presented here. The results contribute a small addition to the data available on the effects of compressibility on secondary flows. Planned measurements will make substantial contributions in that direction in the future.

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 score0.305
Threshold uncertainty score0.381

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 head0.021
GPT teacher head0.214
Teacher spread0.193 · 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
Published2008
Admission routes1
Has abstractyes

Explore more

Same topicTurbomachinery Performance and OptimizationFrench-language works237,207