{"title":"Feasibility Study of Novel Magnetic Compaction Force Assisted Additive Manufacturing (MCFA-AM) Methodology for Continuous Carbon Fiber Reinforced Polymer (C-CFRP) Composites","authors":"B. Ranabhat, S. Kirmse, K. Hsiao","doi":"10.33599/NASAMPE/S.19.1535","DOIUrl":"https://doi.org/10.33599/NASAMPE/S.19.1535","url":null,"abstract":"","PeriodicalId":162077,"journal":{"name":"SAMPE 2019 - Charlotte, NC","volume":"47 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-04-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126340500","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Novel Ultra Low Viscosity Epoxy for Enhancing the Tg and Processability of Multifunctional Thermosets","authors":"Huifeng Qian, P. Badrinarayanan","doi":"10.33599/NASAMPE/S.19.1453","DOIUrl":"https://doi.org/10.33599/NASAMPE/S.19.1453","url":null,"abstract":"","PeriodicalId":162077,"journal":{"name":"SAMPE 2019 - Charlotte, NC","volume":"24 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-04-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121581729","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
S. Shewchuk, B. Halford, M. Matlack, A. Sharpe, Pete Massey
{"title":"Development of Scalable Dynamic Control Architectures for Flexible Composites Manufacturing Work Cells","authors":"S. Shewchuk, B. Halford, M. Matlack, A. Sharpe, Pete Massey","doi":"10.33599/NASAMPE/S.19.1391","DOIUrl":"https://doi.org/10.33599/NASAMPE/S.19.1391","url":null,"abstract":"","PeriodicalId":162077,"journal":{"name":"SAMPE 2019 - Charlotte, NC","volume":"113 2","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-04-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"120941504","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
T. Tsotsis, Gilbert Cespedes-Gonzalez, M. Wiener, Leslie A. Cohen, D. Calamito, S. Costantino, F. Klunker
{"title":"Fabrication of a Complex Part with Deep-Draw Sections By Resin Transfer Molding","authors":"T. Tsotsis, Gilbert Cespedes-Gonzalez, M. Wiener, Leslie A. Cohen, D. Calamito, S. Costantino, F. Klunker","doi":"10.33599/NASAMPE/S.19.1389","DOIUrl":"https://doi.org/10.33599/NASAMPE/S.19.1389","url":null,"abstract":"","PeriodicalId":162077,"journal":{"name":"SAMPE 2019 - Charlotte, NC","volume":"58 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-04-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131120996","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
D MooreJeron, André Colvin, S. Ghose, A JohnsonBrice
{"title":"Design for Manufacturing: Laminate Focused Design and Analysis Tools for Automated Composites Manufacturing","authors":"D MooreJeron, André Colvin, S. Ghose, A JohnsonBrice","doi":"10.33599/NASAMPE/S.19.1478","DOIUrl":"https://doi.org/10.33599/NASAMPE/S.19.1478","url":null,"abstract":"","PeriodicalId":162077,"journal":{"name":"SAMPE 2019 - Charlotte, NC","volume":"2 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-04-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132585788","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Curtis Hickmott, A. Forghani, Victoria Hutten, Evan Lorbiecki, F. Palmieri, B. Grimsley, B. Coxon, G. Fernlund, A. Poursartip
{"title":"A Numerical and Experimental Approach for Modeling Porosity Due to Entrapped Air and Volatiles Off-gassing During Manufacturing of Composite Structures","authors":"Curtis Hickmott, A. Forghani, Victoria Hutten, Evan Lorbiecki, F. Palmieri, B. Grimsley, B. Coxon, G. Fernlund, A. Poursartip","doi":"10.33599/NASAMPE/S.19.1627","DOIUrl":"https://doi.org/10.33599/NASAMPE/S.19.1627","url":null,"abstract":"High performance composite structures have strict requirements regarding acceptable levels of porosity. The impact can be significant on mechanical performance and mitigating the growth of voids can be a challenge given the complexity of the problem. The evolution of porosity can be summarized as a balance between sources and sinks which determine void growth or shrinkage. The primary sources of void growth include bag leaks, entrapped air in the system, off-gassing of volatiles, and cure shrinkage. Mechanisms which mitigate porosity include removal of air from the system and maintaining sufficient resin pressure during the process to keep volatiles in solution. In this paper, an approach for modeling the evolution of voids due to entrapped air and volatiles is presented. It has been shown in previous experimental studies that decreases in local resin pressure are linked to a higher likelihood of porosity formation. Results of the study are compared to experiments in which the local resin pressure was measured and micrographs of the panels were taken to characterize the porosity.","PeriodicalId":162077,"journal":{"name":"SAMPE 2019 - Charlotte, NC","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-04-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114492454","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
C. Henry, K. Rupel, Charles Park, Joseph A. Costanzo, Cary Kaczowka, Kevin F. Malik, S. Ghose
{"title":"Evaluation of an Alternate Method for Determining Yield Strength Offset Values for Selective Laser Sintered Polymeric Materials","authors":"C. Henry, K. Rupel, Charles Park, Joseph A. Costanzo, Cary Kaczowka, Kevin F. Malik, S. Ghose","doi":"10.33599/NASAMPE/S.19.1583","DOIUrl":"https://doi.org/10.33599/NASAMPE/S.19.1583","url":null,"abstract":"Due to the unique characteristics of Additively Manufactured (AM) polymeric materials, typical mechanical strength characterization methods such as those commonly used for traditionally-processed polymers or composite materials can produce results that do not accurately represent material capabilities. In order to characterize mechanical properties of these materials, new test and analysis methods are required. As part of the National Aeronautics and Space Administration (NASA) Advanced Composites Project (ACP), Boeing has evaluated true yield testing as an alternative or complimentary test to 0.2% offset yield testing for determining appropriate yield strength values of polymer materials. Previous testing has shown high strain, low modulus polymer materials such as selective laser sintered (SLS) Nylon 11 at elevated temperatures produce large variations in yield strength. The true yield test method was successful in finding the applied strain level when yield commences and appears to offer an increase in data robustness. The material contained in this paper is based upon work supported by NASA under award No. NNL09AA00A through a sub award from the National Institute of Aerospace.","PeriodicalId":162077,"journal":{"name":"SAMPE 2019 - Charlotte, NC","volume":"11 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-04-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117084923","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}