{"id":{"repo_id":"nps","oai_identifier":"oai:calhoun.nps.edu:10945/13262"},"canonical_url":"https://search.dev.ndltd.org/etd/nps/oai:calhoun.nps.edu:10945/13262","repository":{"repo_id":"nps","name":"Naval Postgraduate School","base_url":"https://calhoun.nps.edu/server/oai/request"},"display":{"title":"A theoretical and experimental study of the impingement of two subsonic jets","abstract":"A theoretical and experimental investigation has been performed on the determination of the characteristics of two impinging plane turbulent jets for the purpose of under1tanding the performance of proportional fluid amplifiers and momentum-exchange devices . The jet deflection angle was determined through the application of the free-streamline theory for two normally impinging jets with arbitrary throat widths and wall set-backs . The deflection angle and the velocity and turbulence distributions acro1s and at various distances along the jet were determined through the use of a hot-wire anemometer system. The results are presented in terms of normalized parameters suitable for comparison with the theoretical predictions. The deflection angles predicted theoretically were found to be in good agreement with those obtained experimentally.","abstract_html":"A theoretical and experimental investigation has been performed on the determination of the characteristics of two impinging plane turbulent jets for the purpose of under1tanding the performance of proportional fluid amplifiers and momentum-exchange devices . The jet deflection angle was determined through the application of the free-streamline theory for two normally impinging jets with arbitrary throat widths and wall set-backs . The deflection angle and the velocity and turbulence distributions acro1s and at various distances along the jet were determined through the use of a hot-wire anemometer system. The results are presented in terms of normalized parameters suitable for comparison with the theoretical predictions. The deflection angles predicted theoretically were found to be in good agreement with those obtained experimentally.","abstract_has_math":false,"creators":["Gungor, Nihat"],"institution":"Monterey, California. U.S. Naval Postgraduate School","degree_name":null,"degree_level":null,"degree_discipline":null,"degree_department":"Mechanical Engineering","school":null,"contributors":[],"advisors":["Sarpkaya, T."],"committee_chairs":[],"committee_members":[],"year":1969,"date_issued":"1969-06","date_published":"1969-06","updated_at":"2026-07-27T20:24:46Z","subjects":[],"languages":["en_US"],"rights":["Copyright is reserved by the copyright owner"],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://hdl.handle.net/10945/13262","outbound_label":"Handle","outbound_source":"dc:identifier.uri"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor.advisor","label":"Advisor","values":["Sarpkaya, T."]},{"key":"dc:contributor.department","label":"Department","values":["Mechanical Engineering"]},{"key":"dc:creator","label":"Author","values":["Gungor, Nihat"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["June 1969"]},{"key":"dc:date.accessioned","label":"Dc Date Accessioned","values":["2012-08-29T23:36:36Z"]},{"key":"dc:date.available","label":"Dc Date Available","values":["2012-08-29T23:36:36Z"]},{"key":"dc:date.issued","label":"Date","values":["1969-06"]},{"key":"dc:publisher","label":"Institution","values":["Monterey, California. U.S. Naval Postgraduate School"]},{"key":"dc:type","label":"Dc Type","values":["Thesis"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:language.iso","label":"Language (ISO)","values":["en_US"]},{"key":"dc:rights","label":"Dc Rights","values":["Copyright is reserved by the copyright owner"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier.uri","label":"Identifier URI","values":["https://hdl.handle.net/10945/13262"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["A theoretical and experimental investigation has been performed on the determination of the characteristics of two impinging plane turbulent jets for the purpose of under1tanding the performance of proportional fluid amplifiers and momentum-exchange devices . The jet deflection angle was determined through the application of the free-streamline theory for two normally impinging jets with arbitrary throat widths and wall set-backs . The deflection angle and the velocity and turbulence distributions acro1s and at various distances along the jet were determined through the use of a hot-wire anemometer system. The results are presented in terms of normalized parameters suitable for comparison with the theoretical predictions. The deflection angles predicted theoretically were found to be in good agreement with those obtained experimentally."]},{"key":"dc:title","label":"Title","values":["A theoretical and experimental study of the impingement of two subsonic jets"]}]}],"canonical_facts":{"dc:contributor.advisor":["Sarpkaya, T."],"dc:contributor.department":["Mechanical Engineering"],"dc:creator":["Gungor, Nihat"],"dc:date":["June 1969"],"dc:date.accessioned":["2012-08-29T23:36:36Z"],"dc:date.available":["2012-08-29T23:36:36Z"],"dc:date.issued":["1969-06"],"dc:description.abstract":["A theoretical and experimental investigation has been performed on the determination of the characteristics of two impinging plane turbulent jets for the purpose of under1tanding the performance of proportional fluid amplifiers and momentum-exchange devices . The jet deflection angle was determined through the application of the free-streamline theory for two normally impinging jets with arbitrary throat widths and wall set-backs . The deflection angle and the velocity and turbulence distributions acro1s and at various distances along the jet were determined through the use of a hot-wire anemometer system. The results are presented in terms of normalized parameters suitable for comparison with the theoretical predictions. The deflection angles predicted theoretically were found to be in good agreement with those obtained experimentally."],"dc:identifier.uri":["https://hdl.handle.net/10945/13262"],"dc:language.iso":["en_US"],"dc:publisher":["Monterey, California. U.S. Naval Postgraduate School"],"dc:rights":["Copyright is reserved by the copyright owner"],"dc:title":["A theoretical and experimental study of the impingement of two subsonic jets"],"dc:type":["Thesis"]},"updated_at":"2026-07-27T20:24:46Z"}