Experimental evidence of H2/O2 propellants powered rotating detonation waves
The paper presents experimental evidence of continuous detonation in a rotating detonation rocket engine (RDRE) powered by H2/O2 propellants. High-speed chemiluminescence imaging is used to characterize the detonation wave dynamics by introducing a tracer in the hydrogen fuel flow. The results show...
Gespeichert in:
| Veröffentlicht in: | Combustion and flame 2020-04, Vol.214, p.136-138 |
|---|---|
| Hauptverfasser: | , , , , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 138 |
|---|---|
| container_issue | |
| container_start_page | 136 |
| container_title | Combustion and flame |
| container_volume | 214 |
| creator | Sosa, Jonathan Burke, Robert Ahmed, Kareem A. Micka, Daniel J. Bennewitz, John W. Danczyk, Stephen A. Paulson, Eric J. Hargus, William A. |
| description | The paper presents experimental evidence of continuous detonation in a rotating detonation rocket engine (RDRE) powered by H2/O2 propellants. High-speed chemiluminescence imaging is used to characterize the detonation wave dynamics by introducing a tracer in the hydrogen fuel flow. The results show continuous five-wave co-rotating detonations at various equivalence ratios and flow rates demonstrating the potential for H2/O2 propellant based RDREs for upper-stage rocket engines. |
| doi_str_mv | 10.1016/j.combustflame.2019.12.031 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2446296690</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0010218019305838</els_id><sourcerecordid>2420633915</sourcerecordid><originalsourceid>FETCH-LOGICAL-c3471-41e3c503480152a78c65a6b04dd382f588bce2e55a55fa1e57ca9f95545c28303</originalsourceid><addsrcrecordid>eNqNkM1OwzAQhC0EEqXwDhack-7acX64oVIoUqVe4Gy5zgYlSuNgpy28PanKgRucdg8zszsfY7cIMQKmsya2brvZhaFqzZZiAVjEKGKQeMYmqFQaiULgOZsAIEQCc7hkVyE0AJAlUk7YavHZk6-31A2m5bSvS-oscVfxpZitBe-966ltTTcE3rsDeSq5d4MZ6u6dlzS4blxdxw9mT-GaXVSmDXTzM6fs7WnxOl9Gq_Xzy_xhFVmZZBglSNIqkEkOqITJcpsqk24gKUuZi0rl-caSIKWMUpVBUpk1RVUolSgrcglyyu5OueN3HzsKg27cznfjSS2SJBVFmhZ_qASkUhaoRtX9SWW9C8FTpfsRh_FfGkEfGetG_2asj4w1Cj0yHs2PJzONbfc1eR1sfQRY1p7soEtX_yfmG5mfiqQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2420633915</pqid></control><display><type>article</type><title>Experimental evidence of H2/O2 propellants powered rotating detonation waves</title><source>Access via ScienceDirect (Elsevier)</source><creator>Sosa, Jonathan ; Burke, Robert ; Ahmed, Kareem A. ; Micka, Daniel J. ; Bennewitz, John W. ; Danczyk, Stephen A. ; Paulson, Eric J. ; Hargus, William A.</creator><creatorcontrib>Sosa, Jonathan ; Burke, Robert ; Ahmed, Kareem A. ; Micka, Daniel J. ; Bennewitz, John W. ; Danczyk, Stephen A. ; Paulson, Eric J. ; Hargus, William A.</creatorcontrib><description>The paper presents experimental evidence of continuous detonation in a rotating detonation rocket engine (RDRE) powered by H2/O2 propellants. High-speed chemiluminescence imaging is used to characterize the detonation wave dynamics by introducing a tracer in the hydrogen fuel flow. The results show continuous five-wave co-rotating detonations at various equivalence ratios and flow rates demonstrating the potential for H2/O2 propellant based RDREs for upper-stage rocket engines.</description><identifier>ISSN: 0010-2180</identifier><identifier>EISSN: 1556-2921</identifier><identifier>DOI: 10.1016/j.combustflame.2019.12.031</identifier><language>eng</language><publisher>New York: Elsevier Inc</publisher><subject>Chemiluminescence ; Detonation waves ; Flow velocity ; Hydrogen fuels ; Propellants ; Rocket engines ; Rotation ; Upper stage rocket engines</subject><ispartof>Combustion and flame, 2020-04, Vol.214, p.136-138</ispartof><rights>2019</rights><rights>Copyright Elsevier BV Apr 2020</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c3471-41e3c503480152a78c65a6b04dd382f588bce2e55a55fa1e57ca9f95545c28303</citedby><cites>FETCH-LOGICAL-c3471-41e3c503480152a78c65a6b04dd382f588bce2e55a55fa1e57ca9f95545c28303</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.combustflame.2019.12.031$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,780,784,3550,27924,27925,45995</link.rule.ids></links><search><creatorcontrib>Sosa, Jonathan</creatorcontrib><creatorcontrib>Burke, Robert</creatorcontrib><creatorcontrib>Ahmed, Kareem A.</creatorcontrib><creatorcontrib>Micka, Daniel J.</creatorcontrib><creatorcontrib>Bennewitz, John W.</creatorcontrib><creatorcontrib>Danczyk, Stephen A.</creatorcontrib><creatorcontrib>Paulson, Eric J.</creatorcontrib><creatorcontrib>Hargus, William A.</creatorcontrib><title>Experimental evidence of H2/O2 propellants powered rotating detonation waves</title><title>Combustion and flame</title><description>The paper presents experimental evidence of continuous detonation in a rotating detonation rocket engine (RDRE) powered by H2/O2 propellants. High-speed chemiluminescence imaging is used to characterize the detonation wave dynamics by introducing a tracer in the hydrogen fuel flow. The results show continuous five-wave co-rotating detonations at various equivalence ratios and flow rates demonstrating the potential for H2/O2 propellant based RDREs for upper-stage rocket engines.</description><subject>Chemiluminescence</subject><subject>Detonation waves</subject><subject>Flow velocity</subject><subject>Hydrogen fuels</subject><subject>Propellants</subject><subject>Rocket engines</subject><subject>Rotation</subject><subject>Upper stage rocket engines</subject><issn>0010-2180</issn><issn>1556-2921</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNqNkM1OwzAQhC0EEqXwDhack-7acX64oVIoUqVe4Gy5zgYlSuNgpy28PanKgRucdg8zszsfY7cIMQKmsya2brvZhaFqzZZiAVjEKGKQeMYmqFQaiULgOZsAIEQCc7hkVyE0AJAlUk7YavHZk6-31A2m5bSvS-oscVfxpZitBe-966ltTTcE3rsDeSq5d4MZ6u6dlzS4blxdxw9mT-GaXVSmDXTzM6fs7WnxOl9Gq_Xzy_xhFVmZZBglSNIqkEkOqITJcpsqk24gKUuZi0rl-caSIKWMUpVBUpk1RVUolSgrcglyyu5OueN3HzsKg27cznfjSS2SJBVFmhZ_qASkUhaoRtX9SWW9C8FTpfsRh_FfGkEfGetG_2asj4w1Cj0yHs2PJzONbfc1eR1sfQRY1p7soEtX_yfmG5mfiqQ</recordid><startdate>202004</startdate><enddate>202004</enddate><creator>Sosa, Jonathan</creator><creator>Burke, Robert</creator><creator>Ahmed, Kareem A.</creator><creator>Micka, Daniel J.</creator><creator>Bennewitz, John W.</creator><creator>Danczyk, Stephen A.</creator><creator>Paulson, Eric J.</creator><creator>Hargus, William A.</creator><general>Elsevier Inc</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>202004</creationdate><title>Experimental evidence of H2/O2 propellants powered rotating detonation waves</title><author>Sosa, Jonathan ; Burke, Robert ; Ahmed, Kareem A. ; Micka, Daniel J. ; Bennewitz, John W. ; Danczyk, Stephen A. ; Paulson, Eric J. ; Hargus, William A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3471-41e3c503480152a78c65a6b04dd382f588bce2e55a55fa1e57ca9f95545c28303</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Chemiluminescence</topic><topic>Detonation waves</topic><topic>Flow velocity</topic><topic>Hydrogen fuels</topic><topic>Propellants</topic><topic>Rocket engines</topic><topic>Rotation</topic><topic>Upper stage rocket engines</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sosa, Jonathan</creatorcontrib><creatorcontrib>Burke, Robert</creatorcontrib><creatorcontrib>Ahmed, Kareem A.</creatorcontrib><creatorcontrib>Micka, Daniel J.</creatorcontrib><creatorcontrib>Bennewitz, John W.</creatorcontrib><creatorcontrib>Danczyk, Stephen A.</creatorcontrib><creatorcontrib>Paulson, Eric J.</creatorcontrib><creatorcontrib>Hargus, William A.</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Combustion and flame</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Sosa, Jonathan</au><au>Burke, Robert</au><au>Ahmed, Kareem A.</au><au>Micka, Daniel J.</au><au>Bennewitz, John W.</au><au>Danczyk, Stephen A.</au><au>Paulson, Eric J.</au><au>Hargus, William A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental evidence of H2/O2 propellants powered rotating detonation waves</atitle><jtitle>Combustion and flame</jtitle><date>2020-04</date><risdate>2020</risdate><volume>214</volume><spage>136</spage><epage>138</epage><pages>136-138</pages><issn>0010-2180</issn><eissn>1556-2921</eissn><abstract>The paper presents experimental evidence of continuous detonation in a rotating detonation rocket engine (RDRE) powered by H2/O2 propellants. High-speed chemiluminescence imaging is used to characterize the detonation wave dynamics by introducing a tracer in the hydrogen fuel flow. The results show continuous five-wave co-rotating detonations at various equivalence ratios and flow rates demonstrating the potential for H2/O2 propellant based RDREs for upper-stage rocket engines.</abstract><cop>New York</cop><pub>Elsevier Inc</pub><doi>10.1016/j.combustflame.2019.12.031</doi><tpages>3</tpages><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0010-2180 |
| ispartof | Combustion and flame, 2020-04, Vol.214, p.136-138 |
| issn | 0010-2180 1556-2921 |
| language | eng |
| recordid | cdi_proquest_journals_2446296690 |
| source | Access via ScienceDirect (Elsevier) |
| subjects | Chemiluminescence Detonation waves Flow velocity Hydrogen fuels Propellants Rocket engines Rotation Upper stage rocket engines |
| title | Experimental evidence of H2/O2 propellants powered rotating detonation waves |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T23%3A11%3A04IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Experimental%20evidence%20of%20H2/O2%20propellants%20powered%20rotating%20detonation%20waves&rft.jtitle=Combustion%20and%20flame&rft.au=Sosa,%20Jonathan&rft.date=2020-04&rft.volume=214&rft.spage=136&rft.epage=138&rft.pages=136-138&rft.issn=0010-2180&rft.eissn=1556-2921&rft_id=info:doi/10.1016/j.combustflame.2019.12.031&rft_dat=%3Cproquest_cross%3E2420633915%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2420633915&rft_id=info:pmid/&rft_els_id=S0010218019305838&rfr_iscdi=true |