{"doi":"10.1115/1.4012869","title":"The Boundary Layer on the End Wall of a Turbine Nozzle Cascade","abstract":"<jats:title>Abstract</jats:title>\n               <jats:p>The boundary layer flow was experimentally studied on an end wall of a turbine-nozzle cascade and the following results were obtained. 1 The boundary layer was laminar at the throat of the nozzle, even when the upstream boundary layer was apparently turbulent. 2 The end-wall boundary layer in the nozzle was little affected by the upstream boundary layer. A theoretical consideration supports the results and also reveals that the part of secondary flow in the nozzle, which is related to the upstream boundary layer, depends upon the configuration of the nozzle. 3 The observed boundary layer behavior was compared with the predicted flow by a three-dimensional laminar boundary layer theory, and good agreement was obtained. 4 The measurements showed the end-wall boundary layer rolling up at the suction-surface end-wall corner of the cascade. The mechanism of the rolling up is explained.</jats:p>","journal":"Journal of Fluids Engineering","year":1958,"id":26776,"datarank":2.3644825384551913,"base_score":2.772588722239781,"endowment":2.772588722239781,"self_citation_contribution":0.41588830833596724,"citation_network_contribution":1.9485942301192243,"self_endowment_contribution":0.41588830833596724,"citer_contribution":1.9485942301192243,"corpus_percentile":null,"corpus_rank":null,"citation_count":15,"citer_count":15,"citers_with_citation_signal":14,"citers_with_endowment":14,"datacite_reuse_total":0,"is_dataset":false,"is_dataset_confidence":null,"is_data_producer":false,"deposit_databanks":null,"is_oa":false,"file_count":0,"downloads":0,"has_version_chain":false,"published_date":null,"fair_score":null,"fair_percentile":null,"algorithm_id":"datarank_citation_only_1hop_v6","ranking_scope":"data_only","authors":[{"id":154152,"name":"Yasutoshi Senoo","orcid":null,"position":0,"is_corresponding":false}],"reference_count":0,"raw_metadata":{"has_enrichment":true,"base_score":2.772588722239781,"endowment":2.772588722239781,"datacite_reuse_total":0,"file_count":0,"downloads":0,"views":0,"has_version_chain":false,"is_dataset":false,"is_oa":false,"pmid":"18998881","pmcid":null,"openalex_id":"https://openalex.org/W4206926120","authors":[],"funders":[],"total_grants":0,"fwci":9.5507,"citation_percentile":0.97950633,"influential_citations":0,"citation_trend":[{"year":2017,"count":1}],"oa_status":"closed","license":"https://www.asme.org/publications-submissions/publishing-information/legal-policies","oa_locations":[{"url":"https://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/80/8/1711/6826311/1711_1.pdf","host_type":"publisher"},{"url":"https://doi.org/10.1115/1.4012869","host_type":"journal"}],"fields_of_study":["Aerodynamics and Acoustics in Jet Flows","Turbomachinery Performance and Optimization","Fluid Dynamics and Turbulent Flows","Engineering","Physics"],"mesh_terms":[],"keywords":["Boundary layer","Boundary layer suction","Nozzle","Laminar flow","Blasius boundary layer","Boundary layer control","Boundary layer thickness","Mechanics","Cascade","External flow","Materials science","Flow separation","Boundary (topology)","Flow (mathematics)","Physics","Chemistry","Thermodynamics","Mathematics"],"sdg_mappings":[],"linked_datasets":[],"clinical_trials":[],"software_tools":[],"database_accessions":[],"source":"live","citation_network_status":"fetched"},"created_at":"2026-06-08T15:40:16.064410Z","pmid":null,"pmcid":null,"fwci":null,"citation_percentile":null,"influential_citations":0,"oa_status":null,"license":null,"views":0,"total_file_size_bytes":0,"version_count":0,"fair_f":null,"fair_a":null,"fair_i":null,"fair_r":null,"fair_zscore":null,"fair_rationale":null,"fair_model":null,"fair_agent_version":null,"fair_fulltext_source":null,"fair_has_llm":null,"fair_computed_at":null,"clinical_trials":[],"software_tools":[],"db_accessions":[],"linked_datasets":[],"topics":[]}