A unified transition mechanism from shock to detonation waves
The transition of shock-to-detonation is of great significance for the investigation of supernova formation, disaster prevention and supersonic propulsion technology. In this paper, the influence Equation of shock-to-detonation transition is summarized for the oblique detonation problem from aerodyn...
Gespeichert in:
| Hauptverfasser: | , , , , |
|---|---|
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | Yan, Hao Xiong, Haochen Han, Xin Shi, Chongguang You, Yancheng |
| description | The transition of shock-to-detonation is of great significance for the
investigation of supernova formation, disaster prevention and supersonic
propulsion technology. In this paper, the influence Equation of
shock-to-detonation transition is summarized for the oblique detonation problem
from aerodynamic analysis. The Equation integrates the effects of parameters
such as chemical reaction, shock intensity and wall conditions, which
quantitatively explains the physical mechanism of shock-to-detonation
transition in the form of mathematical expression. Comparison with numerical
simulation results as well as their gradients verified the reliability of the
influence Equation. Further, the influence Equation can also be used to predict
the critical conditions for the transition from shock to detonation transition
form. In addition to oblique detonation, the influence Equation is compatible
with the deflagration-to-detonation problem for normal detonation, which shows
a wide applicability. |
| doi_str_mv | 10.48550/arxiv.2408.03042 |
| format | Article |
| fullrecord | <record><control><sourceid>arxiv_GOX</sourceid><recordid>TN_cdi_arxiv_primary_2408_03042</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2408_03042</sourcerecordid><originalsourceid>FETCH-arxiv_primary_2408_030423</originalsourceid><addsrcrecordid>eNpjYJA0NNAzsTA1NdBPLKrILNMzMjGw0DMwNjAx4mSwdVQozctMy0xNUSgpSswrzizJzM9TyE1NzkjMyyzOVUgrys9VKM7IT85WKMlXSEktyc9LBCspTyxLLeZhYE1LzClO5YXS3Azybq4hzh66YIviC4oycxOLKuNBFsaDLTQmrAIAXaM15Q</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>A unified transition mechanism from shock to detonation waves</title><source>arXiv.org</source><creator>Yan, Hao ; Xiong, Haochen ; Han, Xin ; Shi, Chongguang ; You, Yancheng</creator><creatorcontrib>Yan, Hao ; Xiong, Haochen ; Han, Xin ; Shi, Chongguang ; You, Yancheng</creatorcontrib><description>The transition of shock-to-detonation is of great significance for the
investigation of supernova formation, disaster prevention and supersonic
propulsion technology. In this paper, the influence Equation of
shock-to-detonation transition is summarized for the oblique detonation problem
from aerodynamic analysis. The Equation integrates the effects of parameters
such as chemical reaction, shock intensity and wall conditions, which
quantitatively explains the physical mechanism of shock-to-detonation
transition in the form of mathematical expression. Comparison with numerical
simulation results as well as their gradients verified the reliability of the
influence Equation. Further, the influence Equation can also be used to predict
the critical conditions for the transition from shock to detonation transition
form. In addition to oblique detonation, the influence Equation is compatible
with the deflagration-to-detonation problem for normal detonation, which shows
a wide applicability.</description><identifier>DOI: 10.48550/arxiv.2408.03042</identifier><language>eng</language><subject>Physics - Fluid Dynamics</subject><creationdate>2024-08</creationdate><rights>http://creativecommons.org/licenses/by-nc-nd/4.0</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>228,230,776,881</link.rule.ids><linktorsrc>$$Uhttps://arxiv.org/abs/2408.03042$$EView_record_in_Cornell_University$$FView_record_in_$$GCornell_University$$Hfree_for_read</linktorsrc><backlink>$$Uhttps://doi.org/10.48550/arXiv.2408.03042$$DView paper in arXiv$$Hfree_for_read</backlink></links><search><creatorcontrib>Yan, Hao</creatorcontrib><creatorcontrib>Xiong, Haochen</creatorcontrib><creatorcontrib>Han, Xin</creatorcontrib><creatorcontrib>Shi, Chongguang</creatorcontrib><creatorcontrib>You, Yancheng</creatorcontrib><title>A unified transition mechanism from shock to detonation waves</title><description>The transition of shock-to-detonation is of great significance for the
investigation of supernova formation, disaster prevention and supersonic
propulsion technology. In this paper, the influence Equation of
shock-to-detonation transition is summarized for the oblique detonation problem
from aerodynamic analysis. The Equation integrates the effects of parameters
such as chemical reaction, shock intensity and wall conditions, which
quantitatively explains the physical mechanism of shock-to-detonation
transition in the form of mathematical expression. Comparison with numerical
simulation results as well as their gradients verified the reliability of the
influence Equation. Further, the influence Equation can also be used to predict
the critical conditions for the transition from shock to detonation transition
form. In addition to oblique detonation, the influence Equation is compatible
with the deflagration-to-detonation problem for normal detonation, which shows
a wide applicability.</description><subject>Physics - Fluid Dynamics</subject><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>GOX</sourceid><recordid>eNpjYJA0NNAzsTA1NdBPLKrILNMzMjGw0DMwNjAx4mSwdVQozctMy0xNUSgpSswrzizJzM9TyE1NzkjMyyzOVUgrys9VKM7IT85WKMlXSEktyc9LBCspTyxLLeZhYE1LzClO5YXS3Azybq4hzh66YIviC4oycxOLKuNBFsaDLTQmrAIAXaM15Q</recordid><startdate>20240806</startdate><enddate>20240806</enddate><creator>Yan, Hao</creator><creator>Xiong, Haochen</creator><creator>Han, Xin</creator><creator>Shi, Chongguang</creator><creator>You, Yancheng</creator><scope>GOX</scope></search><sort><creationdate>20240806</creationdate><title>A unified transition mechanism from shock to detonation waves</title><author>Yan, Hao ; Xiong, Haochen ; Han, Xin ; Shi, Chongguang ; You, Yancheng</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-arxiv_primary_2408_030423</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Physics - Fluid Dynamics</topic><toplevel>online_resources</toplevel><creatorcontrib>Yan, Hao</creatorcontrib><creatorcontrib>Xiong, Haochen</creatorcontrib><creatorcontrib>Han, Xin</creatorcontrib><creatorcontrib>Shi, Chongguang</creatorcontrib><creatorcontrib>You, Yancheng</creatorcontrib><collection>arXiv.org</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Yan, Hao</au><au>Xiong, Haochen</au><au>Han, Xin</au><au>Shi, Chongguang</au><au>You, Yancheng</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A unified transition mechanism from shock to detonation waves</atitle><date>2024-08-06</date><risdate>2024</risdate><abstract>The transition of shock-to-detonation is of great significance for the
investigation of supernova formation, disaster prevention and supersonic
propulsion technology. In this paper, the influence Equation of
shock-to-detonation transition is summarized for the oblique detonation problem
from aerodynamic analysis. The Equation integrates the effects of parameters
such as chemical reaction, shock intensity and wall conditions, which
quantitatively explains the physical mechanism of shock-to-detonation
transition in the form of mathematical expression. Comparison with numerical
simulation results as well as their gradients verified the reliability of the
influence Equation. Further, the influence Equation can also be used to predict
the critical conditions for the transition from shock to detonation transition
form. In addition to oblique detonation, the influence Equation is compatible
with the deflagration-to-detonation problem for normal detonation, which shows
a wide applicability.</abstract><doi>10.48550/arxiv.2408.03042</doi><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | DOI: 10.48550/arxiv.2408.03042 |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_arxiv_primary_2408_03042 |
| source | arXiv.org |
| subjects | Physics - Fluid Dynamics |
| title | A unified transition mechanism from shock to detonation waves |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-10T01%3A07%3A13IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-arxiv_GOX&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20unified%20transition%20mechanism%20from%20shock%20to%20detonation%20waves&rft.au=Yan,%20Hao&rft.date=2024-08-06&rft_id=info:doi/10.48550/arxiv.2408.03042&rft_dat=%3Carxiv_GOX%3E2408_03042%3C/arxiv_GOX%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |