Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/105971
PIRA download icon_1.1View/Download Full Text
DC FieldValueLanguage
dc.contributorDepartment of Aeronautical and Aviation Engineering-
dc.creatorWen, CYen_US
dc.creatorJiang, Yen_US
dc.creatorShi, Len_US
dc.date.accessioned2024-04-23T04:32:40Z-
dc.date.available2024-04-23T04:32:40Z-
dc.identifier.isbn978-981-99-0875-2 (Hardcover)en_US
dc.identifier.isbn978-981-99-0878-3 (Softcover)en_US
dc.identifier.isbn978-981-99-0876-9 (eBook)en_US
dc.identifier.urihttp://hdl.handle.net/10397/105971-
dc.language.isoenen_US
dc.publisherSpringeren_US
dc.rights© The Editor(s) (if applicable) and The Author(s) 2023. This book is an open access publication.en_US
dc.rightsThis book is licensed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.en_US
dc.rightsThe following publication Wen, CY., Jiang, Y., Shi, L. (2023). Application: Detonations. In: Space–Time Conservation Element and Solution Element Method. Engineering Applications of Computational Methods, vol 13. Springer, Singapore is available at https://doi.org/10.1007/978-981-99-0876-9_8.en_US
dc.titleApplication : detonationsen_US
dc.typeBook Chapteren_US
dc.identifier.spage95en_US
dc.identifier.epage122en_US
dc.identifier.doi10.1007/978-981-99-0876-9_8en_US
dcterms.abstractDetonation is a shock-induced combustion in which chemical reactions are closely coupled with shock waves. The shock wave compresses the reactant with an abrupt increase in temperature and pressure, initiating the reactants to be burnt into products. The intense heat release permits the high propagating speed of the shock wave to be sustained. It is fundamental research related to both the safety industry and propulsion systems. For most explosive mixtures, detonation wave speeds are formulated by Chapman–Jouguet (CJ) theory. Typical detonation velocities for gaseous mixtures generally range from 1400 to 3000 m/s. Behind the shock, the time scale for reactions is commonly on the order of microseconds or even less. Furthermore, the detonation front is intrinsically unstable, forming transient multi-dimensional structures. Many studies revealed that high resolution is necessary to resolve the essential detonation structures. Due to its complex nature and multiple time scales, detonation is thus a challenging problem for solvers on shock-capturing capability, robustness, and computational efficiency. This chapter will present several essential aspects of detonation research by applying the CESE schemes.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationIn CY Wen, Y Jiang, & L Shi (2023), Space-time conservation element and solution element method: advances and applications in engineering sciences, p. 95-122. Singapore: Springer.en_US
dcterms.issued2023-
dc.identifier.scopus2-s2.0-85153030804-
dc.relation.ispartofbookSpace-time conservation element and solution element method : advances and applications in engineering sciencesen_US
dc.publisher.placeSingaporeen_US
dc.description.validate202404 bcch-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Scopus/WOS-
dc.description.fundingSourceSelf-fundeden_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryCCen_US
Appears in Collections:Book Chapter
Files in This Item:
File Description SizeFormat 
978-981-99-0876-9_8.pdf1.3 MBAdobe PDFView/Open
Open Access Information
Status open access
File Version Version of Record
Access
View full-text via PolyU eLinks SFX Query
Show simple item record

Page views

4
Citations as of May 12, 2024

Google ScholarTM

Check

Altmetric


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.