Characterization of Detonation Phenomena Observed in High-Speed Visible Imagery
Measurements for radius, angular velocity, initial time of observation, and final time of observation were made for turbulent vortices around detonation fireballs. A proxy for vortex power, determined through unit analysis, was found to correlate well to initial (and final) time of observation with...
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description | Measurements for radius, angular velocity, initial time of observation, and final time of observation were made for turbulent vortices around detonation fireballs. A proxy for vortex power, determined through unit analysis, was found to correlate well to initial (and final) time of observation with R(exp 2) equal to 0.8572. The linear trend on a log(sub 10)-log(sub 10) plot was indicative of a rapid decrease (over 10(exp -1 s)) in power associated with the decay of the fireball. Predictions, based on turbulent spectral theory were made for root-mean-square velocity fluctuations and Reynolds numbers, both as functions of time. In addition, reflected shock speeds inside the fireball were found to be, on average, 69% higher than those of the un-reflected shock outside. This difference in speed was used to estimate the adiabatic exponent inside the fireball. Values of the adiabatic exponent were found to range between 1.08 and 1.3, while exhibiting a decreasing trend in time, and a weak quadratic dependence on time. Lastly, comparisons of the primary and secondary shock velocities showed that the secondary shock was faster in eight out of ten events. For the remaining two events, the speeds were equal to within the uncertainty of the measurements. The speed of the secondary shock varied from 1.8% to 30% faster than the primary shock. |
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A proxy for vortex power, determined through unit analysis, was found to correlate well to initial (and final) time of observation with R(exp 2) equal to 0.8572. The linear trend on a log(sub 10)-log(sub 10) plot was indicative of a rapid decrease (over 10(exp -1 s)) in power associated with the decay of the fireball. Predictions, based on turbulent spectral theory were made for root-mean-square velocity fluctuations and Reynolds numbers, both as functions of time. In addition, reflected shock speeds inside the fireball were found to be, on average, 69% higher than those of the un-reflected shock outside. This difference in speed was used to estimate the adiabatic exponent inside the fireball. Values of the adiabatic exponent were found to range between 1.08 and 1.3, while exhibiting a decreasing trend in time, and a weak quadratic dependence on time. Lastly, comparisons of the primary and secondary shock velocities showed that the secondary shock was faster in eight out of ten events. For the remaining two events, the speeds were equal to within the uncertainty of the measurements. The speed of the secondary shock varied from 1.8% to 30% faster than the primary shock.</description><language>eng</language><subject>Acoustics ; ADIABATIC EXPONENTS ; Ammunition and Explosives ; ANGULAR VELOCITY ; COST EFFECTIVENESS ; DETONATIONS ; EXPLOSIONS ; Fluid Mechanics ; IMAGE PROCESSING ; LOW STRENGTH ; Miscellaneous Detection and Detectors ; NUCLEAR FIREBALL ; QUADRATIC EQUATIONS ; REFLECTION ; REMOTE DETECTION ; REYNOLDS NUMBER ; SATELLITE IMAGERY ; SHOCK WAVES ; SPECTRA ; THEORY ; THESES ; TURBULENCE ; UNCERTAINTY ; VELOCITY ; VORTICES</subject><creationdate>2006</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA450096$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Warren, Trevor W</creatorcontrib><creatorcontrib>AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING AND MANAGEMENT</creatorcontrib><title>Characterization of Detonation Phenomena Observed in High-Speed Visible Imagery</title><description>Measurements for radius, angular velocity, initial time of observation, and final time of observation were made for turbulent vortices around detonation fireballs. A proxy for vortex power, determined through unit analysis, was found to correlate well to initial (and final) time of observation with R(exp 2) equal to 0.8572. The linear trend on a log(sub 10)-log(sub 10) plot was indicative of a rapid decrease (over 10(exp -1 s)) in power associated with the decay of the fireball. Predictions, based on turbulent spectral theory were made for root-mean-square velocity fluctuations and Reynolds numbers, both as functions of time. In addition, reflected shock speeds inside the fireball were found to be, on average, 69% higher than those of the un-reflected shock outside. This difference in speed was used to estimate the adiabatic exponent inside the fireball. Values of the adiabatic exponent were found to range between 1.08 and 1.3, while exhibiting a decreasing trend in time, and a weak quadratic dependence on time. Lastly, comparisons of the primary and secondary shock velocities showed that the secondary shock was faster in eight out of ten events. For the remaining two events, the speeds were equal to within the uncertainty of the measurements. The speed of the secondary shock varied from 1.8% to 30% faster than the primary shock.</description><subject>Acoustics</subject><subject>ADIABATIC EXPONENTS</subject><subject>Ammunition and Explosives</subject><subject>ANGULAR VELOCITY</subject><subject>COST EFFECTIVENESS</subject><subject>DETONATIONS</subject><subject>EXPLOSIONS</subject><subject>Fluid Mechanics</subject><subject>IMAGE PROCESSING</subject><subject>LOW STRENGTH</subject><subject>Miscellaneous Detection and Detectors</subject><subject>NUCLEAR FIREBALL</subject><subject>QUADRATIC EQUATIONS</subject><subject>REFLECTION</subject><subject>REMOTE DETECTION</subject><subject>REYNOLDS NUMBER</subject><subject>SATELLITE IMAGERY</subject><subject>SHOCK WAVES</subject><subject>SPECTRA</subject><subject>THEORY</subject><subject>THESES</subject><subject>TURBULENCE</subject><subject>UNCERTAINTY</subject><subject>VELOCITY</subject><subject>VORTICES</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>2006</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZPB3zkgsSkwuSS3KrEosyczPU8hPU3BJLcnPg_ACMlLz8nNT8xIV_JOKU4vKUlMUMvMUPDLTM3SDC1KBvLDM4syknFQFz9zE9NSiSh4G1rTEnOJUXijNzSDj5hri7KGbUpKZHF9ckpmXWhLv6OJoYmpgYGlmTEAaAB96M70</recordid><startdate>200603</startdate><enddate>200603</enddate><creator>Warren, Trevor W</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>200603</creationdate><title>Characterization of Detonation Phenomena Observed in High-Speed Visible Imagery</title><author>Warren, Trevor W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA4500963</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>2006</creationdate><topic>Acoustics</topic><topic>ADIABATIC EXPONENTS</topic><topic>Ammunition and Explosives</topic><topic>ANGULAR VELOCITY</topic><topic>COST EFFECTIVENESS</topic><topic>DETONATIONS</topic><topic>EXPLOSIONS</topic><topic>Fluid Mechanics</topic><topic>IMAGE PROCESSING</topic><topic>LOW STRENGTH</topic><topic>Miscellaneous Detection and Detectors</topic><topic>NUCLEAR FIREBALL</topic><topic>QUADRATIC EQUATIONS</topic><topic>REFLECTION</topic><topic>REMOTE DETECTION</topic><topic>REYNOLDS NUMBER</topic><topic>SATELLITE IMAGERY</topic><topic>SHOCK WAVES</topic><topic>SPECTRA</topic><topic>THEORY</topic><topic>THESES</topic><topic>TURBULENCE</topic><topic>UNCERTAINTY</topic><topic>VELOCITY</topic><topic>VORTICES</topic><toplevel>online_resources</toplevel><creatorcontrib>Warren, Trevor W</creatorcontrib><creatorcontrib>AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING AND MANAGEMENT</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Warren, Trevor W</au><aucorp>AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING AND MANAGEMENT</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Characterization of Detonation Phenomena Observed in High-Speed Visible Imagery</btitle><date>2006-03</date><risdate>2006</risdate><abstract>Measurements for radius, angular velocity, initial time of observation, and final time of observation were made for turbulent vortices around detonation fireballs. A proxy for vortex power, determined through unit analysis, was found to correlate well to initial (and final) time of observation with R(exp 2) equal to 0.8572. The linear trend on a log(sub 10)-log(sub 10) plot was indicative of a rapid decrease (over 10(exp -1 s)) in power associated with the decay of the fireball. Predictions, based on turbulent spectral theory were made for root-mean-square velocity fluctuations and Reynolds numbers, both as functions of time. In addition, reflected shock speeds inside the fireball were found to be, on average, 69% higher than those of the un-reflected shock outside. This difference in speed was used to estimate the adiabatic exponent inside the fireball. Values of the adiabatic exponent were found to range between 1.08 and 1.3, while exhibiting a decreasing trend in time, and a weak quadratic dependence on time. Lastly, comparisons of the primary and secondary shock velocities showed that the secondary shock was faster in eight out of ten events. For the remaining two events, the speeds were equal to within the uncertainty of the measurements. The speed of the secondary shock varied from 1.8% to 30% faster than the primary shock.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | Acoustics ADIABATIC EXPONENTS Ammunition and Explosives ANGULAR VELOCITY COST EFFECTIVENESS DETONATIONS EXPLOSIONS Fluid Mechanics IMAGE PROCESSING LOW STRENGTH Miscellaneous Detection and Detectors NUCLEAR FIREBALL QUADRATIC EQUATIONS REFLECTION REMOTE DETECTION REYNOLDS NUMBER SATELLITE IMAGERY SHOCK WAVES SPECTRA THEORY THESES TURBULENCE UNCERTAINTY VELOCITY VORTICES |
title | Characterization of Detonation Phenomena Observed in High-Speed Visible Imagery |
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