{"id":{"repo_id":"carleton","oai_identifier":"oai:carleton.scholaris.ca:20.500.14718/27274"},"canonical_url":"https://search.dev.ndltd.org/etd/carleton/oai:carleton.scholaris.ca:20.500.14718/27274","repository":{"repo_id":"carleton","name":"Carleton University","base_url":"https://carleton.scholaris.ca/server/oai/request"},"display":{"title":"The Numerical solution of the radial-equilibrium equation for swirling flow in arbitrarily shaped ducts","abstract":"The radial-equilibrium equation is discussed with regard to turbomachinery. The complete equation is derived for nonviscous flow and the simplifications are indicated. Five different techniques for the solution of three-dimensional compressible flow in a duct are examined in detail. A comparison with M. Vavra's results (11) is given for an accelerating bend with axisymmetric flow. The inlet to an annular wind tunnel is examined for different swirl velocities. Listings of the programs and printed output are included.","abstract_html":"The radial-equilibrium equation is discussed with regard to turbomachinery. The complete equation is derived for nonviscous flow and the simplifications are indicated. Five different techniques for the solution of three-dimensional compressible flow in a duct are examined in detail. A comparison with M. Vavra's results (11) is given for an accelerating bend with axisymmetric flow. The inlet to an annular wind tunnel is examined for different swirl velocities. Listings of the programs and printed output are included.","abstract_has_math":false,"creators":["Davis, Willard Roland"],"institution":"Carleton University","degree_name":"Master of Engineering (M.Eng.)","degree_level":"Master's","degree_discipline":"Engineering, Mechanical","degree_department":null,"school":null,"contributors":[],"advisors":[],"committee_chairs":[],"committee_members":[],"year":1967,"date_issued":"1967","date_published":"1967","updated_at":"2026-07-24T01:34:45Z","subjects":[],"languages":["en"],"rights":["Copyright © 1967 the author(s). Theses may be used for non-commercial research, educational, or related academic purposes only. Such uses include personal study, research, scholarship, and teaching. Theses may only be shared by linking to Carleton University Institutional Repository and no part may be used without proper attribution to the author. 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The complete equation is derived for nonviscous flow and the simplifications are indicated. Five different techniques for the solution of three-dimensional compressible flow in a duct are examined in detail. A comparison with M. Vavra's results (11) is given for an accelerating bend with axisymmetric flow. The inlet to an annular wind tunnel is examined for different swirl velocities. Listings of the programs and printed output are included."]},{"key":"dc:title","label":"Title","values":["The Numerical solution of the radial-equilibrium equation for swirling flow in arbitrarily shaped ducts"]}]}],"canonical_facts":{"dc:creator":["Davis, Willard Roland"],"dc:date.accessioned":["2025-04-08T16:25:27Z"],"dc:date.available":["2025-04-08T16:25:27Z"],"dc:date.issued":["1967"],"dc:description.abstract":["The radial-equilibrium equation is discussed with regard to turbomachinery. The complete equation is derived for nonviscous flow and the simplifications are indicated. 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