Resin shrinkage due to chemical changes and thermal gradients plays an important role in the residual stress evolution during composite manufacturing. In this thesis, we develop a new in-situ experimental approach for measuring resin shrinkage during curing with the help of digital image correlation (DIC) instrumented on a specially designed autoclave with borosilicate viewports. The images of the resin sample are captured at regular intervals with the help of DIC to measure the displacement and strains during the curing process. We utilize this method for a comparative analysis of resin shrinkage in two common aerospace epoxies, Epoxy 105 and EPON 862. An average compressive strain of 0.00896 was observed for Epoxy 105 and 0.01042 for EPON 862. Differential Scanning Calorimeter (DSC) is used to measure the degree of cure for the two epoxies, and to correlate resin shrinkage to the cure state. We also observed the effect of fibers on the shrinkage of the resin using carbon fiber, glass fiber and crepe bandage as fillers. We observed that as the stiffness of the fillers increased the strain in the matrix decreased.
","abstract_html":"<p>Resin shrinkage due to chemical changes and thermal gradients plays an important role in the residual stress evolution during composite manufacturing. In this thesis, we develop a new in-situ experimental approach for measuring resin shrinkage during curing with the help of digital image correlation (DIC) instrumented on a specially designed autoclave with borosilicate viewports. The images of the resin sample are captured at regular intervals with the help of DIC to measure the displacement and strains during the curing process. We utilize this method for a comparative analysis of resin shrinkage in two common aerospace epoxies, Epoxy 105 and EPON 862. An average compressive strain of 0.00896 was observed for Epoxy 105 and 0.01042 for EPON 862. Differential Scanning Calorimeter (DSC) is used to measure the degree of cure for the two epoxies, and to correlate resin shrinkage to the cure state. We also observed the effect of fibers on the shrinkage of the resin using carbon fiber, glass fiber and crepe bandage as fillers. We observed that as the stiffness of the fillers increased the strain in the matrix decreased.</p>","abstract_has_math":false,"creators":["Motagi, Samarth"],"institution":null,"degree_name":"Master of Science in Aerospace Engineering","degree_level":"Thesis - Open Access","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":[],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2019,"date_issued":"2019-12-01T08:00:00Z","date_published":"2019-12-01T08:00:00Z","updated_at":"2026-07-27T19:25:37Z","subjects":["in-situ","resin","shrinkage","aerospace","Aerospace Engineering","Structures and Materials"],"languages":[],"rights":[],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://commons.erau.edu/edt/491","outbound_label":"Repository record","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:creator","label":"Author","values":["Motagi, Samarth"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"thesis:degree_discipline","label":"Discipline","values":["Aerospace Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Thesis - Open Access"]},{"key":"thesis:degree_name","label":"Degree Name","values":["Master of Science in Aerospace Engineering"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["in-situ","resin","shrinkage","aerospace","Aerospace Engineering","Structures and Materials"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://commons.erau.edu/edt/491"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["Resin shrinkage due to chemical changes and thermal gradients plays an important role in the residual stress evolution during composite manufacturing. In this thesis, we develop a new in-situ experimental approach for measuring resin shrinkage during curing with the help of digital image correlation (DIC) instrumented on a specially designed autoclave with borosilicate viewports. The images of the resin sample are captured at regular intervals with the help of DIC to measure the displacement and strains during the curing process. We utilize this method for a comparative analysis of resin shrinkage in two common aerospace epoxies, Epoxy 105 and EPON 862. An average compressive strain of 0.00896 was observed for Epoxy 105 and 0.01042 for EPON 862. Differential Scanning Calorimeter (DSC) is used to measure the degree of cure for the two epoxies, and to correlate resin shrinkage to the cure state. We also observed the effect of fibers on the shrinkage of the resin using carbon fiber, glass fiber and crepe bandage as fillers. We observed that as the stiffness of the fillers increased the strain in the matrix decreased.
"]},{"key":"dc:title","label":"Title","values":["In-Situ Measurement of Resin Shrinkage for Aerospace Components"]}]}],"canonical_facts":{"dc:creator":["Motagi, Samarth"],"dc:description.abstract":["Resin shrinkage due to chemical changes and thermal gradients plays an important role in the residual stress evolution during composite manufacturing. In this thesis, we develop a new in-situ experimental approach for measuring resin shrinkage during curing with the help of digital image correlation (DIC) instrumented on a specially designed autoclave with borosilicate viewports. The images of the resin sample are captured at regular intervals with the help of DIC to measure the displacement and strains during the curing process. We utilize this method for a comparative analysis of resin shrinkage in two common aerospace epoxies, Epoxy 105 and EPON 862. An average compressive strain of 0.00896 was observed for Epoxy 105 and 0.01042 for EPON 862. Differential Scanning Calorimeter (DSC) is used to measure the degree of cure for the two epoxies, and to correlate resin shrinkage to the cure state. We also observed the effect of fibers on the shrinkage of the resin using carbon fiber, glass fiber and crepe bandage as fillers. We observed that as the stiffness of the fillers increased the strain in the matrix decreased.
"],"dc:identifier":["https://commons.erau.edu/edt/491"],"dc:subject":["in-situ","resin","shrinkage","aerospace","Aerospace Engineering","Structures and Materials"],"dc:title":["In-Situ Measurement of Resin Shrinkage for Aerospace Components"],"thesis:degree_discipline":["Aerospace Engineering"],"thesis:degree_level":["Thesis - Open Access"],"thesis:degree_name":["Master of Science in Aerospace Engineering"]},"updated_at":"2026-07-27T19:25:37Z"}