{"id":{"repo_id":"vt","oai_identifier":"oai:vtechworks.lib.vt.edu:10919/30854"},"canonical_url":"https://search.dev.ndltd.org/etd/vt/oai:vtechworks.lib.vt.edu:10919/30854","repository":{"repo_id":"vt","name":"Virginia Tech","base_url":"https://vtechworks.lib.vt.edu/oai/request"},"display":{"title":"Measurements and Predictions of Heat Transfer for a First Vane Design","abstract":"Turbine manufacturers continually seek to gain efficiency by increasing operating temperatures well above the maximum temperature of component alloys. This increase in temperature must be accounted for in the cooling of components by examining the heat transfer from these crucial components. This study specifically examines the effect of a contoured endwall on the heat transfer of a scaled-up stator vane. Understanding the three-dimensional effects of contoured endwalls on vane heat transfer can lead to prolonging blade life. The results of a combined experimental and computational study of heat transfer along the surface of a turbine vane that incorporates a contoured endwall are discussed in detail. A commercially available computational fluid dynamics code was used to design a contoured endwall and simulate an engine representative pressure distribution for a turbine vane cascade placed in a low-speed wind tunnel. A significant flow acceleration caused by the contour increased heat transfer over 40% of the vane span compared to the vane far from the contoured endwall. The effects of freestream turbulence with respect to the contour were examined. Results showed a significant increase in heat transfer at elevated freestream turbulence levels at each span location. The effects of the contour were minimal compared to the effects of increased turbulence. The boundary layer transition location moved further upstream with increasing turbulence. Trip wires were used to model the effect of film-cooling holes on the boundary layer development. The heat transfer increased locally at the trip and either remained elevated if the boundary layer remained turbulent or the heat transfer decreased as the boundary layer relaminarized due to flow acceleration. These results are beneficial to turbine manufacturers interested in effective placement of film-cooling holes.","abstract_html":"Turbine manufacturers continually seek to gain efficiency by increasing operating temperatures well above the maximum temperature of component alloys. This increase in temperature must be accounted for in the cooling of components by examining the heat transfer from these crucial components. This study specifically examines the effect of a contoured endwall on the heat transfer of a scaled-up stator vane. Understanding the three-dimensional effects of contoured endwalls on vane heat transfer can lead to prolonging blade life. The results of a combined experimental and computational study of heat transfer along the surface of a turbine vane that incorporates a contoured endwall are discussed in detail. A commercially available computational fluid dynamics code was used to design a contoured endwall and simulate an engine representative pressure distribution for a turbine vane cascade placed in a low-speed wind tunnel. A significant flow acceleration caused by the contour increased heat transfer over 40% of the vane span compared to the vane far from the contoured endwall. The effects of freestream turbulence with respect to the contour were examined. Results showed a significant increase in heat transfer at elevated freestream turbulence levels at each span location. The effects of the contour were minimal compared to the effects of increased turbulence. The boundary layer transition location moved further upstream with increasing turbulence. Trip wires were used to model the effect of film-cooling holes on the boundary layer development. The heat transfer increased locally at the trip and either remained elevated if the boundary layer remained turbulent or the heat transfer decreased as the boundary layer relaminarized due to flow acceleration. These results are beneficial to turbine manufacturers interested in effective placement of film-cooling holes.","abstract_has_math":false,"creators":["Gratton, Andrew Robert"],"institution":"Virginia Tech","degree_name":"Master of Science","degree_level":"masters","degree_discipline":"Mechanical Engineering","degree_department":"Mechanical Engineering","school":null,"contributors":[],"advisors":[],"committee_chairs":["Thole, Karen A."],"committee_members":["Vick, Brian L.","Ng, Fai"],"year":2004,"date_issued":"2004-01-06","date_published":"2004-01-06","updated_at":"2026-07-22T22:19:22Z","subjects":["gas turbines","Heat--Transmission"],"languages":[],"rights":["In Copyright"],"rights_urls":["http://rightsstatements.org/vocab/InC/1.0/"],"identifier_entries":[{"key":"dc:identifier.other","label":"Dc Identifier Other","values":["etd-01082004-161821"],"render_values":[{"text":"etd-01082004-161821","href":null,"code":true}]}]},"links":{"outbound_url":"http://hdl.handle.net/10919/30854","outbound_label":"Handle","outbound_source":"dc:identifier.uri"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor.committeechair","label":"Committee Chair","values":["Thole, Karen A."]},{"key":"dc:contributor.committeemember","label":"Committee Member","values":["Vick, Brian L.","Ng, Fai"]},{"key":"dc:contributor.department","label":"Department","values":["Mechanical Engineering"]},{"key":"dc:creator","label":"Author","values":["Gratton, Andrew Robert"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date.accessioned","label":"Dc Date Accessioned","values":["2014-03-14T20:30:17Z"]},{"key":"dc:date.available","label":"Dc Date Available","values":["2014-03-14T20:30:17Z","2005-01-22"]},{"key":"dc:date.issued","label":"Date","values":["2004-01-06"]},{"key":"dc:publisher","label":"Institution","values":["Virginia Tech"]},{"key":"dc:type","label":"Dc Type","values":["Thesis"]},{"key":"thesis:degree_discipline","label":"Discipline","values":["Mechanical Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["masters"]},{"key":"thesis:degree_name","label":"Degree Name","values":["Master of Science"]},{"key":"thesis:institution_name","label":"Thesis Institution Name","values":["Virginia Polytechnic Institute and State University"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["gas turbines","Heat--Transmission"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:rights","label":"Dc Rights","values":["In Copyright"]},{"key":"dc:rights.uri","label":"Rights URI","values":["http://rightsstatements.org/vocab/InC/1.0/"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier.other","label":"Dc Identifier Other","values":["etd-01082004-161821"]},{"key":"dc:identifier.uri","label":"Identifier URI","values":["http://hdl.handle.net/10919/30854"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["Turbine manufacturers continually seek to gain efficiency by increasing operating temperatures well above the maximum temperature of component alloys. This increase in temperature must be accounted for in the cooling of components by examining the heat transfer from these crucial components. This study specifically examines the effect of a contoured endwall on the heat transfer of a scaled-up stator vane. Understanding the three-dimensional effects of contoured endwalls on vane heat transfer can lead to prolonging blade life. The results of a combined experimental and computational study of heat transfer along the surface of a turbine vane that incorporates a contoured endwall are discussed in detail. A commercially available computational fluid dynamics code was used to design a contoured endwall and simulate an engine representative pressure distribution for a turbine vane cascade placed in a low-speed wind tunnel. A significant flow acceleration caused by the contour increased heat transfer over 40% of the vane span compared to the vane far from the contoured endwall. The effects of freestream turbulence with respect to the contour were examined. Results showed a significant increase in heat transfer at elevated freestream turbulence levels at each span location. The effects of the contour were minimal compared to the effects of increased turbulence. The boundary layer transition location moved further upstream with increasing turbulence. Trip wires were used to model the effect of film-cooling holes on the boundary layer development. The heat transfer increased locally at the trip and either remained elevated if the boundary layer remained turbulent or the heat transfer decreased as the boundary layer relaminarized due to flow acceleration. These results are beneficial to turbine manufacturers interested in effective placement of film-cooling holes."]},{"key":"dc:description.degree","label":"Dc Description Degree","values":["Master of Science"]},{"key":"dc:title","label":"Title","values":["Measurements and Predictions of Heat Transfer for a First Vane Design"]}]}],"canonical_facts":{"dc:contributor.committeechair":["Thole, Karen A."],"dc:contributor.committeemember":["Vick, Brian L.","Ng, Fai"],"dc:contributor.department":["Mechanical Engineering"],"dc:creator":["Gratton, Andrew Robert"],"dc:date.accessioned":["2014-03-14T20:30:17Z"],"dc:date.available":["2014-03-14T20:30:17Z","2005-01-22"],"dc:date.issued":["2004-01-06"],"dc:description.abstract":["Turbine manufacturers continually seek to gain efficiency by increasing operating temperatures well above the maximum temperature of component alloys. This increase in temperature must be accounted for in the cooling of components by examining the heat transfer from these crucial components. This study specifically examines the effect of a contoured endwall on the heat transfer of a scaled-up stator vane. Understanding the three-dimensional effects of contoured endwalls on vane heat transfer can lead to prolonging blade life. The results of a combined experimental and computational study of heat transfer along the surface of a turbine vane that incorporates a contoured endwall are discussed in detail. A commercially available computational fluid dynamics code was used to design a contoured endwall and simulate an engine representative pressure distribution for a turbine vane cascade placed in a low-speed wind tunnel. A significant flow acceleration caused by the contour increased heat transfer over 40% of the vane span compared to the vane far from the contoured endwall. The effects of freestream turbulence with respect to the contour were examined. Results showed a significant increase in heat transfer at elevated freestream turbulence levels at each span location. The effects of the contour were minimal compared to the effects of increased turbulence. The boundary layer transition location moved further upstream with increasing turbulence. Trip wires were used to model the effect of film-cooling holes on the boundary layer development. The heat transfer increased locally at the trip and either remained elevated if the boundary layer remained turbulent or the heat transfer decreased as the boundary layer relaminarized due to flow acceleration. These results are beneficial to turbine manufacturers interested in effective placement of film-cooling holes."],"dc:description.degree":["Master of Science"],"dc:identifier.other":["etd-01082004-161821"],"dc:identifier.uri":["http://hdl.handle.net/10919/30854"],"dc:publisher":["Virginia Tech"],"dc:rights":["In Copyright"],"dc:rights.uri":["http://rightsstatements.org/vocab/InC/1.0/"],"dc:subject":["gas turbines","Heat--Transmission"],"dc:title":["Measurements and Predictions of Heat Transfer for a First Vane Design"],"dc:type":["Thesis"],"thesis:degree_discipline":["Mechanical Engineering"],"thesis:degree_level":["masters"],"thesis:degree_name":["Master of Science"],"thesis:institution_name":["Virginia Polytechnic Institute and State University"]},"updated_at":"2026-07-22T22:19:22Z"}