{"id":{"repo_id":"nps","oai_identifier":"oai:calhoun.nps.edu:10945/18365"},"canonical_url":"https://search.dev.ndltd.org/etd/nps/oai:calhoun.nps.edu:10945/18365","repository":{"repo_id":"nps","name":"Naval Postgraduate School","base_url":"https://calhoun.nps.edu/server/oai/request"},"display":{"title":"Cascade wind tunnel for transonic compressor blading studies.","abstract":"The design and construction of a small, transonic, cascade wind tunnel are reported. The tunnel is of the intermittent blow-down type, and the initial test cascade models the flow at the rotor blade tips of a single stage transonic compressor at a relative Mach number of 1.U-. General programs were developed for the design of round-torectangular transition sections and for the computation of supersonic nozzle contours. Complete machine drawings for the important components of the facility are included.","abstract_html":"The design and construction of a small, transonic, cascade wind tunnel are reported. The tunnel is of the intermittent blow-down type, and the initial test cascade models the flow at the rotor blade tips of a single stage transonic compressor at a relative Mach number of 1.U-. General programs were developed for the design of round-torectangular transition sections and for the computation of supersonic nozzle contours. Complete machine drawings for the important components of the facility are included.","abstract_has_math":false,"creators":["Demo, Willard Joe"],"institution":null,"degree_name":null,"degree_level":null,"degree_discipline":null,"degree_department":"Mechanical Engineering","school":null,"contributors":[],"advisors":["Shreeve, R.P."],"committee_chairs":[],"committee_members":[],"year":1978,"date_issued":"1978","date_published":"1978","updated_at":"2026-07-27T20:26:05Z","subjects":[],"languages":["en_US"],"rights":["This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. 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Complete machine drawings for the important components of the facility are included."]},{"key":"dc:title","label":"Title","values":["Cascade wind tunnel for transonic compressor blading studies."]}]}],"canonical_facts":{"dc:contributor.advisor":["Shreeve, R.P."],"dc:contributor.department":["Mechanical Engineering"],"dc:creator":["Demo, Willard Joe"],"dc:date":["June 1978"],"dc:date.accessioned":["2012-11-16T19:21:10Z"],"dc:date.available":["2012-11-16T19:21:10Z"],"dc:date.issued":["1978"],"dc:description.abstract":["The design and construction of a small, transonic, cascade wind tunnel are reported. The tunnel is of the intermittent blow-down type, and the initial test cascade models the flow at the rotor blade tips of a single stage transonic compressor at a relative Mach number of 1.U-. General programs were developed for the design of round-torectangular transition sections and for the computation of supersonic nozzle contours. 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