Please use this identifier to cite or link to this item:
http://hdl.handle.net/10397/78671
DC Field | Value | Language |
---|---|---|
dc.contributor | Department of Mechanical Engineering | - |
dc.creator | Shen, H | - |
dc.creator | Wen, CY | - |
dc.date.accessioned | 2018-09-28T01:17:15Z | - |
dc.date.available | 2018-09-28T01:17:15Z | - |
dc.identifier.uri | http://hdl.handle.net/10397/78671 | - |
dc.language.iso | en | en_US |
dc.publisher | Elsevier | en_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.rights | The 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.subject | Gas dynamics | en_US |
dc.subject | Supersonic/hypersonic flow | en_US |
dc.subject | Shock stand-off distance | en_US |
dc.subject | Non-equilibrium flow | en_US |
dc.subject | Blunt body shock | en_US |
dc.title | Theoretical investigation of shock stand-off distance for non-equilibrium flows over spheres | en_US |
dc.type | Journal/Magazine Article | en_US |
dc.identifier.spage | 990 | - |
dc.identifier.epage | 996 | - |
dc.identifier.volume | 31 | - |
dc.identifier.issue | 5 | - |
dc.identifier.doi | 10.1016/j.cja.2018.02.013 | - |
dcterms.abstract | We 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.accessRights | open access | en_US |
dcterms.bibliographicCitation | Chinese journal of aeronautics, May 2018, v. 31, no. 5, p. 990-996 | - |
dcterms.isPartOf | Chinese journal of aeronautics | - |
dcterms.issued | 2018 | - |
dc.identifier.isi | WOS:000432486800010 | - |
dc.identifier.scopus | 2-s2.0-85044997688 | - |
dc.identifier.eissn | 1000-9361 | - |
dc.identifier.rosgroupid | 2017000443 | - |
dc.description.ros | 2017-2018 > Academic research: refereed > Publication in refereed journal | - |
dc.description.validate | 201809 bcrc | - |
dc.description.oa | Version of Record | en_US |
dc.identifier.FolderNumber | OA_IR/PIRA | en_US |
dc.description.pubStatus | Published | en_US |
Appears in Collections: | Journal/Magazine Article |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
Shen_Shock_Stand-off_Distance.pdf | 751.81 kB | Adobe PDF | View/Open |
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