{"id":{"repo_id":"uiuc","oai_identifier":"oai:www.ideals.illinois.edu:2142/120146"},"canonical_url":"https://search.dev.ndltd.org/etd/uiuc/oai:www.ideals.illinois.edu:2142/120146","repository":{"repo_id":"uiuc","name":"University of Illinois - Urbana-Champaign","base_url":"https://www.ideals.illinois.edu/oai-pmh"},"display":{"title":"Force and moment analysis of a passive morphing wing under unsteady motion","abstract":"Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-09-01 without embargo terms","abstract_html":"Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-09-01 without embargo terms","abstract_has_math":false,"creators":["Namdeo, Kuldeep"],"institution":"University of Illinois at Urbana-Champaign","degree_name":"M.S.","degree_level":"Thesis","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":["Saxton-Fox, Theresa"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2023,"date_issued":"2023-05","date_published":"2023-05","updated_at":"2026-07-22T22:24:56Z","subjects":["Unsteady Aerodynamics","Morphing Wing"],"languages":["en","eng"],"rights":["Copyright 2023 Kuldeep Namdeo"],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://hdl.handle.net/2142/120146","outbound_label":"Handle","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Saxton-Fox, Theresa"]},{"key":"dc:creator","label":"Author","values":["Namdeo, Kuldeep"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["2023-05","2023-05-03"]},{"key":"dc:type","label":"Dc Type","values":["text"]},{"key":"thesis:degree_discipline","label":"Discipline","values":["Aerospace Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Thesis"]},{"key":"thesis:degree_name","label":"Degree Name","values":["M.S."]},{"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":["Unsteady Aerodynamics","Morphing Wing"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:language","label":"Dc Language","values":["en","eng"]},{"key":"dc:rights","label":"Dc Rights","values":["Copyright 2023 Kuldeep Namdeo"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://hdl.handle.net/2142/120146"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description","label":"Description","values":["Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-09-01 without embargo terms","The student, Kuldeep Namdeo, accepted the attached license on 2023-04-28 at 15:58.","The student, Kuldeep Namdeo, submitted this Thesis for approval on 2023-04-28 at 17:10.","This Thesis was approved for publication on 2023-05-03 at 09:04.","DSpace SAF Submission Ingestion Package generated from Vireo submission #19257 on 2023-09-01 at 16:56:00","An experimental setup is designed to provide unsteady linear and rotational motion to a wing and measure aerodynamic loading. A passive morphing wing configuration is studied in the current work with a bi-stable trailing edge that can snap through instabilities to two different configurations. This passive morphing is capable of toggling to different configurations based on the perceived pressure field. A load cell is used to measure forces and moments on the wing. The objectives of the overall study are: (i) To develop and characterize an experimental setup for future unsteady aerodynamics studies. (ii) To determine the aerodynamic loading experienced by the wing and capture the dynamic loading experienced during the snap-through process. (iii) To understand the performance of the morphing under varied conditions to enable improved iterations of the wing. The current study will focus on results from load cell measurements for both static and passively morphing airfoils."]},{"key":"dc:format","label":"Dc Format","values":["application/pdf"]},{"key":"dc:title","label":"Title","values":["Force and moment analysis of a passive morphing wing under unsteady motion"]}]}],"canonical_facts":{"dc:contributor":["Saxton-Fox, Theresa"],"dc:creator":["Namdeo, Kuldeep"],"dc:date":["2023-05","2023-05-03"],"dc:description":["Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-09-01 without embargo terms","The student, Kuldeep Namdeo, accepted the attached license on 2023-04-28 at 15:58.","The student, Kuldeep Namdeo, submitted this Thesis for approval on 2023-04-28 at 17:10.","This Thesis was approved for publication on 2023-05-03 at 09:04.","DSpace SAF Submission Ingestion Package generated from Vireo submission #19257 on 2023-09-01 at 16:56:00","An experimental setup is designed to provide unsteady linear and rotational motion to a wing and measure aerodynamic loading. A passive morphing wing configuration is studied in the current work with a bi-stable trailing edge that can snap through instabilities to two different configurations. This passive morphing is capable of toggling to different configurations based on the perceived pressure field. A load cell is used to measure forces and moments on the wing. The objectives of the overall study are: (i) To develop and characterize an experimental setup for future unsteady aerodynamics studies. (ii) To determine the aerodynamic loading experienced by the wing and capture the dynamic loading experienced during the snap-through process. (iii) To understand the performance of the morphing under varied conditions to enable improved iterations of the wing. The current study will focus on results from load cell measurements for both static and passively morphing airfoils."],"dc:format":["application/pdf"],"dc:identifier":["https://hdl.handle.net/2142/120146"],"dc:language":["en","eng"],"dc:rights":["Copyright 2023 Kuldeep Namdeo"],"dc:subject":["Unsteady Aerodynamics","Morphing Wing"],"dc:title":["Force and moment analysis of a passive morphing wing under unsteady motion"],"dc:type":["text"],"thesis:degree_discipline":["Aerospace Engineering"],"thesis:degree_level":["Thesis"],"thesis:degree_name":["M.S."],"thesis:institution_name":["University of Illinois at Urbana-Champaign"]},"updated_at":"2026-07-22T22:24:56Z"}