{"id":{"repo_id":"uiuc","oai_identifier":"oai:www.ideals.illinois.edu:2142/70119"},"canonical_url":"https://search.dev.ndltd.org/etd/uiuc/oai:www.ideals.illinois.edu:2142/70119","repository":{"repo_id":"uiuc","name":"University of Illinois - Urbana-Champaign","base_url":"https://www.ideals.illinois.edu/oai-pmh"},"display":{"title":"A Study of an Asymmetric Two-Dimensional Nozzle as A Vector-Thrust Device","abstract":"The problem of compressible flow through an asymmetric two-dimensional convergent nozzle is solved by employing the method of hodograph transformation, coupled with finite-difference computation. With the given appropriate flow parameters, solution of the flow problem is first established in the hodograph domain. The corresponding nozzle configuration and local flowfield properties are subsequently obtained through direct integration. Vector-thrust performance and configuration design under certain constraints are also presented. Wind tunnel experiments are also conducted to obtain pressure data along the nozzle walls for verification purposes. The numerical results are found to be in good agreement with the measured data.","abstract_html":"The problem of compressible flow through an asymmetric two-dimensional convergent nozzle is solved by employing the method of hodograph transformation, coupled with finite-difference computation. With the given appropriate flow parameters, solution of the flow problem is first established in the hodograph domain. The corresponding nozzle configuration and local flowfield properties are subsequently obtained through direct integration. Vector-thrust performance and configuration design under certain constraints are also presented. Wind tunnel experiments are also conducted to obtain pressure data along the nozzle walls for verification purposes. The numerical results are found to be in good agreement with the measured data.","abstract_has_math":false,"creators":["Wu, Chivey Chi Wai"],"institution":"University of Illinois at Urbana-Champaign","degree_name":"Ph.D.","degree_level":"Dissertation","degree_discipline":"Mechanical Engineering","degree_department":null,"school":null,"contributors":[],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2014,"date_issued":"2014-12-15T21:41:12Z","date_published":"2014-12-15T21:41:12Z","updated_at":"2026-07-22T22:26:02Z","subjects":["Engineering, Mechanical"],"languages":[],"rights":[],"rights_urls":[],"identifier_entries":[{"key":"dc:identifier","label":"Identifier","values":["(UMI)AAI8410075"],"render_values":[{"text":"(UMI)AAI8410075","href":null,"code":true}]}]},"links":{"outbound_url":"http://hdl.handle.net/2142/70119","outbound_label":"Handle","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:creator","label":"Author","values":["Wu, Chivey Chi Wai"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["2014-12-15T21:41:12Z","10000-01-01","1983"]},{"key":"dc:type","label":"Dc Type","values":["text"]},{"key":"thesis:degree_discipline","label":"Discipline","values":["Mechanical Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Dissertation"]},{"key":"thesis:degree_name","label":"Degree Name","values":["Ph.D."]},{"key":"thesis:institution_name","label":"Thesis Institution Name","values":["University of Illinois at Urbana-Champaign"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["Engineering, Mechanical"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["http://hdl.handle.net/2142/70119","(UMI)AAI8410075"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description","label":"Description","values":["The problem of compressible flow through an asymmetric two-dimensional convergent nozzle is solved by employing the method of hodograph transformation, coupled with finite-difference computation. With the given appropriate flow parameters, solution of the flow problem is first established in the hodograph domain. The corresponding nozzle configuration and local flowfield properties are subsequently obtained through direct integration. Vector-thrust performance and configuration design under certain constraints are also presented. Wind tunnel experiments are also conducted to obtain pressure data along the nozzle walls for verification purposes. The numerical results are found to be in good agreement with the measured data.","Made available in DSpace on 2014-12-15T21:41:12Z (GMT). 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With the given appropriate flow parameters, solution of the flow problem is first established in the hodograph domain. The corresponding nozzle configuration and local flowfield properties are subsequently obtained through direct integration. Vector-thrust performance and configuration design under certain constraints are also presented. Wind tunnel experiments are also conducted to obtain pressure data along the nozzle walls for verification purposes. The numerical results are found to be in good agreement with the measured data.","Made available in DSpace on 2014-12-15T21:41:12Z (GMT). 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