{"id":{"repo_id":"uiuc","oai_identifier":"oai:www.ideals.illinois.edu:2142/122079"},"canonical_url":"https://search.dev.ndltd.org/etd/uiuc/oai:www.ideals.illinois.edu:2142/122079","repository":{"repo_id":"uiuc","name":"University of Illinois - Urbana-Champaign","base_url":"https://www.ideals.illinois.edu/oai-pmh"},"display":{"title":"Applications of an immersed boundary method on two-dimensional flows at low Reynolds numbers","abstract":"Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2024-03-01 without embargo terms","abstract_html":"Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2024-03-01 without embargo terms","abstract_has_math":false,"creators":["Alhussaini, Mohammad Abdullah H"],"institution":"University of Illinois at Urbana-Champaign","degree_name":"M.S.","degree_level":"Thesis","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":["Bodony, Daniel J"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2023,"date_issued":"2023-12","date_published":"2023-12","updated_at":"2026-07-22T22:25:00Z","subjects":["Immersed Boundary Method","Ibm","Ibpm","Viscous Flow","Low Reynolds Number"],"languages":["en","eng"],"rights":["Copyright 2023 Mohammad Alhussaini"],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://hdl.handle.net/2142/122079","outbound_label":"Handle","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Bodony, Daniel J"]},{"key":"dc:creator","label":"Author","values":["Alhussaini, Mohammad Abdullah H"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date","label":"Dc Date","values":["2023-12","2023-12-08"]},{"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":["Immersed Boundary Method","Ibm","Ibpm","Viscous Flow","Low Reynolds Number"]}]},{"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 Mohammad Alhussaini"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://hdl.handle.net/2142/122079"]}]},{"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 2024-03-01 without embargo terms","The student, Mohammad Alhussaini, accepted the attached license on 2023-12-08 at 13:19.","The student, Mohammad Alhussaini, submitted this Thesis for approval on 2023-12-08 at 13:36.","This Thesis was approved for publication on 2023-12-08 at 14:07.","DSpace SAF Submission Ingestion Package generated from Vireo submission #20183 on 2024-03-01 at 13:15:35","The goal of this work is to investigate the application of the immersed boundary projection method to moving and deforming bodies using the ViscousFlow numerical package [1]. A brief overview discussing the method is presented. Three cases of verification are performed for a stationary NACA0012 at Re = 1000, a sinusoidally plunging NACA0012 at Re = 1000, and a canonical pitch-hold-return flat plate maneuver at Re = 100. The results of the first and third cases were in rough agreement, while the sinusoidally plunging case captured the general frequency of the solution with a noticeable discrepancy. A deformation case with a NACA 4-digit airfoil changing thickness from NACA0006 to NACA0012 at zero angle of attack was also performed. The airfoil starts as a NACA0006 from convective time t = 0 to 5 /∞, where c is the chord and ∞ the freestream velocity. Then, the linear deformation occurs for t = 5 to 10. At t = 10, the airfoil is a NACA0012 and stays stationary until t = 15. In additional simulations, the effect of changing the deformation duration was changed to have duration times of 5, 3, and 1. This work is intended to serve as a base for future work involving investigating morphing shapes used in flow control."]},{"key":"dc:format","label":"Dc Format","values":["application/pdf"]},{"key":"dc:title","label":"Title","values":["Applications of an immersed boundary method on two-dimensional flows at low Reynolds numbers"]}]}],"canonical_facts":{"dc:contributor":["Bodony, Daniel J"],"dc:creator":["Alhussaini, Mohammad Abdullah H"],"dc:date":["2023-12","2023-12-08"],"dc:description":["Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2024-03-01 without embargo terms","The student, Mohammad Alhussaini, accepted the attached license on 2023-12-08 at 13:19.","The student, Mohammad Alhussaini, submitted this Thesis for approval on 2023-12-08 at 13:36.","This Thesis was approved for publication on 2023-12-08 at 14:07.","DSpace SAF Submission Ingestion Package generated from Vireo submission #20183 on 2024-03-01 at 13:15:35","The goal of this work is to investigate the application of the immersed boundary projection method to moving and deforming bodies using the ViscousFlow numerical package [1]. A brief overview discussing the method is presented. Three cases of verification are performed for a stationary NACA0012 at Re = 1000, a sinusoidally plunging NACA0012 at Re = 1000, and a canonical pitch-hold-return flat plate maneuver at Re = 100. The results of the first and third cases were in rough agreement, while the sinusoidally plunging case captured the general frequency of the solution with a noticeable discrepancy. A deformation case with a NACA 4-digit airfoil changing thickness from NACA0006 to NACA0012 at zero angle of attack was also performed. The airfoil starts as a NACA0006 from convective time t = 0 to 5 /∞, where c is the chord and ∞ the freestream velocity. Then, the linear deformation occurs for t = 5 to 10. At t = 10, the airfoil is a NACA0012 and stays stationary until t = 15. In additional simulations, the effect of changing the deformation duration was changed to have duration times of 5, 3, and 1. This work is intended to serve as a base for future work involving investigating morphing shapes used in flow control."],"dc:format":["application/pdf"],"dc:identifier":["https://hdl.handle.net/2142/122079"],"dc:language":["en","eng"],"dc:rights":["Copyright 2023 Mohammad Alhussaini"],"dc:subject":["Immersed Boundary Method","Ibm","Ibpm","Viscous Flow","Low Reynolds Number"],"dc:title":["Applications of an immersed boundary method on two-dimensional flows at low Reynolds numbers"],"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":"2026-07-22T22:25:00Z"}