Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles
Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonat...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Fedorov, A. V. [verfasserIn] |
|---|
| Format: |
Artikel |
|---|---|
| Sprache: |
Englisch |
| Erschienen: |
2013 |
|---|
| Schlagwörter: |
|---|
| Anmerkung: |
© Pleiades Publishing, Ltd. 2013 |
|---|
| Übergeordnetes Werk: |
Enthalten in: Combustion, explosion and shock waves - SP MAIK Nauka/Interperiodica, 1966, 49(2013), 3 vom: Mai, Seite 335-347 |
|---|---|
| Übergeordnetes Werk: |
volume:49 ; year:2013 ; number:3 ; month:05 ; pages:335-347 |
| Links: |
|---|
| DOI / URN: |
10.1134/S0010508213030106 |
|---|
| Katalog-ID: |
OLC2072184517 |
|---|
| LEADER | 01000caa a22002652 4500 | ||
|---|---|---|---|
| 001 | OLC2072184517 | ||
| 003 | DE-627 | ||
| 005 | 20230503022730.0 | ||
| 007 | tu | ||
| 008 | 200819s2013 xx ||||| 00| ||eng c | ||
| 024 | 7 | |a 10.1134/S0010508213030106 |2 doi | |
| 035 | |a (DE-627)OLC2072184517 | ||
| 035 | |a (DE-He213)S0010508213030106-p | ||
| 040 | |a DE-627 |b ger |c DE-627 |e rakwb | ||
| 041 | |a eng | ||
| 082 | 0 | 4 | |a 660 |q VZ |
| 100 | 1 | |a Fedorov, A. V. |e verfasserin |4 aut | |
| 245 | 1 | 0 | |a Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles |
| 264 | 1 | |c 2013 | |
| 336 | |a Text |b txt |2 rdacontent | ||
| 337 | |a ohne Hilfsmittel zu benutzen |b n |2 rdamedia | ||
| 338 | |a Band |b nc |2 rdacarrier | ||
| 500 | |a © Pleiades Publishing, Ltd. 2013 | ||
| 520 | |a Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. | ||
| 650 | 4 | |a gas suspension | |
| 650 | 4 | |a heterogeneous detonation | |
| 650 | 4 | |a detonation suppression by inert particles | |
| 650 | 4 | |a numerical simulation | |
| 700 | 1 | |a Kratova, Yu. V. |4 aut | |
| 773 | 0 | 8 | |i Enthalten in |t Combustion, explosion and shock waves |d SP MAIK Nauka/Interperiodica, 1966 |g 49(2013), 3 vom: Mai, Seite 335-347 |w (DE-627)12959282X |w (DE-600)240334-1 |w (DE-576)015085570 |x 0010-5082 |7 nnns |
| 773 | 1 | 8 | |g volume:49 |g year:2013 |g number:3 |g month:05 |g pages:335-347 |
| 856 | 4 | 1 | |u https://doi.org/10.1134/S0010508213030106 |z lizenzpflichtig |3 Volltext |
| 912 | |a GBV_USEFLAG_A | ||
| 912 | |a SYSFLAG_A | ||
| 912 | |a GBV_OLC | ||
| 912 | |a SSG-OLC-TEC | ||
| 912 | |a SSG-OLC-PHY | ||
| 912 | |a SSG-OLC-CHE | ||
| 912 | |a GBV_ILN_70 | ||
| 912 | |a GBV_ILN_4700 | ||
| 951 | |a AR | ||
| 952 | |d 49 |j 2013 |e 3 |c 05 |h 335-347 | ||
| author_variant |
a v f av avf y v k yv yvk |
|---|---|
| matchkey_str |
article:00105082:2013----::acltoodtntowvpoaainngsupninflm |
| hierarchy_sort_str |
2013 |
| publishDate |
2013 |
| allfields |
10.1134/S0010508213030106 doi (DE-627)OLC2072184517 (DE-He213)S0010508213030106-p DE-627 ger DE-627 rakwb eng 660 VZ Fedorov, A. V. verfasserin aut Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2013 Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. gas suspension heterogeneous detonation detonation suppression by inert particles numerical simulation Kratova, Yu. V. aut Enthalten in Combustion, explosion and shock waves SP MAIK Nauka/Interperiodica, 1966 49(2013), 3 vom: Mai, Seite 335-347 (DE-627)12959282X (DE-600)240334-1 (DE-576)015085570 0010-5082 nnns volume:49 year:2013 number:3 month:05 pages:335-347 https://doi.org/10.1134/S0010508213030106 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE GBV_ILN_70 GBV_ILN_4700 AR 49 2013 3 05 335-347 |
| spelling |
10.1134/S0010508213030106 doi (DE-627)OLC2072184517 (DE-He213)S0010508213030106-p DE-627 ger DE-627 rakwb eng 660 VZ Fedorov, A. V. verfasserin aut Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2013 Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. gas suspension heterogeneous detonation detonation suppression by inert particles numerical simulation Kratova, Yu. V. aut Enthalten in Combustion, explosion and shock waves SP MAIK Nauka/Interperiodica, 1966 49(2013), 3 vom: Mai, Seite 335-347 (DE-627)12959282X (DE-600)240334-1 (DE-576)015085570 0010-5082 nnns volume:49 year:2013 number:3 month:05 pages:335-347 https://doi.org/10.1134/S0010508213030106 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE GBV_ILN_70 GBV_ILN_4700 AR 49 2013 3 05 335-347 |
| allfields_unstemmed |
10.1134/S0010508213030106 doi (DE-627)OLC2072184517 (DE-He213)S0010508213030106-p DE-627 ger DE-627 rakwb eng 660 VZ Fedorov, A. V. verfasserin aut Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2013 Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. gas suspension heterogeneous detonation detonation suppression by inert particles numerical simulation Kratova, Yu. V. aut Enthalten in Combustion, explosion and shock waves SP MAIK Nauka/Interperiodica, 1966 49(2013), 3 vom: Mai, Seite 335-347 (DE-627)12959282X (DE-600)240334-1 (DE-576)015085570 0010-5082 nnns volume:49 year:2013 number:3 month:05 pages:335-347 https://doi.org/10.1134/S0010508213030106 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE GBV_ILN_70 GBV_ILN_4700 AR 49 2013 3 05 335-347 |
| allfieldsGer |
10.1134/S0010508213030106 doi (DE-627)OLC2072184517 (DE-He213)S0010508213030106-p DE-627 ger DE-627 rakwb eng 660 VZ Fedorov, A. V. verfasserin aut Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2013 Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. gas suspension heterogeneous detonation detonation suppression by inert particles numerical simulation Kratova, Yu. V. aut Enthalten in Combustion, explosion and shock waves SP MAIK Nauka/Interperiodica, 1966 49(2013), 3 vom: Mai, Seite 335-347 (DE-627)12959282X (DE-600)240334-1 (DE-576)015085570 0010-5082 nnns volume:49 year:2013 number:3 month:05 pages:335-347 https://doi.org/10.1134/S0010508213030106 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE GBV_ILN_70 GBV_ILN_4700 AR 49 2013 3 05 335-347 |
| allfieldsSound |
10.1134/S0010508213030106 doi (DE-627)OLC2072184517 (DE-He213)S0010508213030106-p DE-627 ger DE-627 rakwb eng 660 VZ Fedorov, A. V. verfasserin aut Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles 2013 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2013 Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. gas suspension heterogeneous detonation detonation suppression by inert particles numerical simulation Kratova, Yu. V. aut Enthalten in Combustion, explosion and shock waves SP MAIK Nauka/Interperiodica, 1966 49(2013), 3 vom: Mai, Seite 335-347 (DE-627)12959282X (DE-600)240334-1 (DE-576)015085570 0010-5082 nnns volume:49 year:2013 number:3 month:05 pages:335-347 https://doi.org/10.1134/S0010508213030106 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE GBV_ILN_70 GBV_ILN_4700 AR 49 2013 3 05 335-347 |
| language |
English |
| source |
Enthalten in Combustion, explosion and shock waves 49(2013), 3 vom: Mai, Seite 335-347 volume:49 year:2013 number:3 month:05 pages:335-347 |
| sourceStr |
Enthalten in Combustion, explosion and shock waves 49(2013), 3 vom: Mai, Seite 335-347 volume:49 year:2013 number:3 month:05 pages:335-347 |
| format_phy_str_mv |
Article |
| institution |
findex.gbv.de |
| topic_facet |
gas suspension heterogeneous detonation detonation suppression by inert particles numerical simulation |
| dewey-raw |
660 |
| isfreeaccess_bool |
false |
| container_title |
Combustion, explosion and shock waves |
| authorswithroles_txt_mv |
Fedorov, A. V. @@aut@@ Kratova, Yu. V. @@aut@@ |
| publishDateDaySort_date |
2013-05-01T00:00:00Z |
| hierarchy_top_id |
12959282X |
| dewey-sort |
3660 |
| id |
OLC2072184517 |
| language_de |
englisch |
| fullrecord |
<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">OLC2072184517</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230503022730.0</controlfield><controlfield tag="007">tu</controlfield><controlfield tag="008">200819s2013 xx ||||| 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1134/S0010508213030106</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)OLC2072184517</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-He213)S0010508213030106-p</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">660</subfield><subfield code="q">VZ</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Fedorov, A. V.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2013</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Pleiades Publishing, Ltd. 2013</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">gas suspension</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">heterogeneous detonation</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">detonation suppression by inert particles</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">numerical simulation</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Kratova, Yu. V.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Combustion, explosion and shock waves</subfield><subfield code="d">SP MAIK Nauka/Interperiodica, 1966</subfield><subfield code="g">49(2013), 3 vom: Mai, Seite 335-347</subfield><subfield code="w">(DE-627)12959282X</subfield><subfield code="w">(DE-600)240334-1</subfield><subfield code="w">(DE-576)015085570</subfield><subfield code="x">0010-5082</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:49</subfield><subfield code="g">year:2013</subfield><subfield code="g">number:3</subfield><subfield code="g">month:05</subfield><subfield code="g">pages:335-347</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1134/S0010508213030106</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_OLC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-TEC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-PHY</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-CHE</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4700</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">49</subfield><subfield code="j">2013</subfield><subfield code="e">3</subfield><subfield code="c">05</subfield><subfield code="h">335-347</subfield></datafield></record></collection>
|
| author |
Fedorov, A. V. |
| spellingShingle |
Fedorov, A. V. ddc 660 misc gas suspension misc heterogeneous detonation misc detonation suppression by inert particles misc numerical simulation Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles |
| authorStr |
Fedorov, A. V. |
| ppnlink_with_tag_str_mv |
@@773@@(DE-627)12959282X |
| format |
Article |
| dewey-ones |
660 - Chemical engineering |
| delete_txt_mv |
keep |
| author_role |
aut aut |
| collection |
OLC |
| remote_str |
false |
| illustrated |
Not Illustrated |
| issn |
0010-5082 |
| topic_title |
660 VZ Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles gas suspension heterogeneous detonation detonation suppression by inert particles numerical simulation |
| topic |
ddc 660 misc gas suspension misc heterogeneous detonation misc detonation suppression by inert particles misc numerical simulation |
| topic_unstemmed |
ddc 660 misc gas suspension misc heterogeneous detonation misc detonation suppression by inert particles misc numerical simulation |
| topic_browse |
ddc 660 misc gas suspension misc heterogeneous detonation misc detonation suppression by inert particles misc numerical simulation |
| format_facet |
Aufsätze Gedruckte Aufsätze |
| format_main_str_mv |
Text Zeitschrift/Artikel |
| carriertype_str_mv |
nc |
| hierarchy_parent_title |
Combustion, explosion and shock waves |
| hierarchy_parent_id |
12959282X |
| dewey-tens |
660 - Chemical engineering |
| hierarchy_top_title |
Combustion, explosion and shock waves |
| isfreeaccess_txt |
false |
| familylinks_str_mv |
(DE-627)12959282X (DE-600)240334-1 (DE-576)015085570 |
| title |
Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles |
| ctrlnum |
(DE-627)OLC2072184517 (DE-He213)S0010508213030106-p |
| title_full |
Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles |
| author_sort |
Fedorov, A. V. |
| journal |
Combustion, explosion and shock waves |
| journalStr |
Combustion, explosion and shock waves |
| lang_code |
eng |
| isOA_bool |
false |
| dewey-hundreds |
600 - Technology |
| recordtype |
marc |
| publishDateSort |
2013 |
| contenttype_str_mv |
txt |
| container_start_page |
335 |
| author_browse |
Fedorov, A. V. Kratova, Yu. V. |
| container_volume |
49 |
| class |
660 VZ |
| format_se |
Aufsätze |
| author-letter |
Fedorov, A. V. |
| doi_str_mv |
10.1134/S0010508213030106 |
| dewey-full |
660 |
| title_sort |
calculation of detonation wave propagation in a gas suspension of aluminum and inert particles |
| title_auth |
Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles |
| abstract |
Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. © Pleiades Publishing, Ltd. 2013 |
| abstractGer |
Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. © Pleiades Publishing, Ltd. 2013 |
| abstract_unstemmed |
Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined. © Pleiades Publishing, Ltd. 2013 |
| collection_details |
GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY SSG-OLC-CHE GBV_ILN_70 GBV_ILN_4700 |
| container_issue |
3 |
| title_short |
Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles |
| url |
https://doi.org/10.1134/S0010508213030106 |
| remote_bool |
false |
| author2 |
Kratova, Yu. V. |
| author2Str |
Kratova, Yu. V. |
| ppnlink |
12959282X |
| mediatype_str_mv |
n |
| isOA_txt |
false |
| hochschulschrift_bool |
false |
| doi_str |
10.1134/S0010508213030106 |
| up_date |
2024-07-03T13:56:47.730Z |
| _version_ |
1803566456747589632 |
| fullrecord_marcxml |
<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">OLC2072184517</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230503022730.0</controlfield><controlfield tag="007">tu</controlfield><controlfield tag="008">200819s2013 xx ||||| 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1134/S0010508213030106</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)OLC2072184517</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-He213)S0010508213030106-p</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">660</subfield><subfield code="q">VZ</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Fedorov, A. V.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Calculation of detonation wave propagation in a gas suspension of aluminum and inert particles</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2013</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Pleiades Publishing, Ltd. 2013</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract Propagation of a detonation wave in a plane channel filled by a gas suspension of fine aluminum particles and inert particles in oxygen is studied. Heterogeneous detonation of aluminum particles in oxygen propagates in the Chapman-Jouguet regime. Two types of the flow resulting from detonation interaction with a cloud of particles are found: continuous propagation with a smaller detonation velocity and flow with detonation failure. The influence of physical and spatial parameters of the inert component of the cloud on these regimes is found, including the mechanism of suppression of heterogeneous detonation, which means separation of the ignition and combustion wave from the leading shock front. Dependences of the velocity deficit on the mass fraction and size of inert particles are determined.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">gas suspension</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">heterogeneous detonation</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">detonation suppression by inert particles</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">numerical simulation</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Kratova, Yu. V.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Combustion, explosion and shock waves</subfield><subfield code="d">SP MAIK Nauka/Interperiodica, 1966</subfield><subfield code="g">49(2013), 3 vom: Mai, Seite 335-347</subfield><subfield code="w">(DE-627)12959282X</subfield><subfield code="w">(DE-600)240334-1</subfield><subfield code="w">(DE-576)015085570</subfield><subfield code="x">0010-5082</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:49</subfield><subfield code="g">year:2013</subfield><subfield code="g">number:3</subfield><subfield code="g">month:05</subfield><subfield code="g">pages:335-347</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1134/S0010508213030106</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_OLC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-TEC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-PHY</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-CHE</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4700</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">49</subfield><subfield code="j">2013</subfield><subfield code="e">3</subfield><subfield code="c">05</subfield><subfield code="h">335-347</subfield></datafield></record></collection>
|
| score |
7.399126 |