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dc.contributor.authorZhao, Wei
dc.contributor.authorKapania, Rakesh K.
dc.date.accessioned2021-11-29T21:21:27Z
dc.date.available2021-11-29T21:21:27Z
dc.date.issued2021-03
dc.identifieroksd_zhao_skinstringerassembly_2021
dc.identifier.citationZhao, W., & Kapania, R. K. (2021, March). Skin-stringer assembly using radial basis functions for curvilinearly stiffened panels. American Institute of Aeronautics and Astronautics Journal, 59(3). https://doi.org/10.2514/1.J059364
dc.identifier.urihttps://hdl.handle.net/11244/331277
dc.descriptionThis is a preprint of an article whose final version has been published in the American Institute of Aeronautics and Astronautics (AIAA) Journal, AIAA, March 2021.
dc.formatapplication/pdf
dc.languageen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.rightsThis material has been previously published. In the Oklahoma State University Library's institutional repository this version is made available through the open access principles and the terms of agreement/consent between the author(s) and the publisher. The permission policy on the use, reproduction or distribution of the material falls under fair use for educational, scholarship, and research purposes. Contact Digital Resources and Discovery Services at lib-dls@okstate.edu or 405-744-9161 for further information.
dc.titleSkin-stringer assembly using radial basis functions for curvilinearly stiffened panels
osu.filenameoksd_zhao_skinstringerassembly_2021.pdf
dc.identifier.doi10.2514/1.J059364
dc.description.departmentMechanical and Aerospace Engineering
dc.type.genreArticle
dc.type.materialText
osu.authorOrcid.urihttp://orcid.org/0000-0002-9105-7322


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