Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/78671
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dc.contributorDepartment of Mechanical Engineering-
dc.creatorShen, H-
dc.creatorWen, CY-
dc.date.accessioned2018-09-28T01:17:15Z-
dc.date.available2018-09-28T01:17:15Z-
dc.identifier.urihttp://hdl.handle.net/10397/78671-
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.rights© 2018 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier B.V. This is an open access article under the CC BY-NC-ND license (http://creativ commons.org/licenses/by-nc-nd/4.0/)-
dc.rightsThe following publication SHEN, H., & WEN, C. -. (2018). Theoretical investigation of shock stand-off distance for non-equilibrium flows over spheres. Chinese Journal of Aeronautics, 31(5), 990-996 is available at https://dx.doi.org/10.1016/j.cja.2018.02.013-
dc.subjectGas dynamicsen_US
dc.subjectSupersonic/hypersonic flowen_US
dc.subjectShock stand-off distanceen_US
dc.subjectNon-equilibrium flowen_US
dc.subjectBlunt body shocken_US
dc.titleTheoretical investigation of shock stand-off distance for non-equilibrium flows over spheresen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage990-
dc.identifier.epage996-
dc.identifier.volume31-
dc.identifier.issue5-
dc.identifier.doi10.1016/j.cja.2018.02.013-
dcterms.abstractWe derived a theoretical solution of the shock stand-off distance for a non-equilibrium flow over spheres based on Wen and Hornung's solution and Olivier's solution. Compared with previous approaches, the main advantage of the present approach is allowing an analytic solution without involving any semi-empirical parameter for the whole non-equilibrium flow regimes. The effects of some important physical quantities therefore can be fully revealed via the analytic solution. By combining the current solution with Ideal Dissociating Gas (IDG) model, we investigate the effects of free stream kinetic energy and free stream dissociation level (which can be very different between different facilities) on the shock stand-off distance.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationChinese journal of aeronautics, May 2018, v. 31, no. 5, p. 990-996-
dcterms.isPartOfChinese journal of aeronautics-
dcterms.issued2018-
dc.identifier.isiWOS:000432486800010-
dc.identifier.scopus2-s2.0-85044997688-
dc.identifier.eissn1000-9361-
dc.identifier.rosgroupid2017000443-
dc.description.ros2017-2018 > Academic research: refereed > Publication in refereed journal-
dc.description.validate201809 bcrc-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_IR/PIRAen_US
dc.description.pubStatusPublisheden_US
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