Computational and Experimental Studies of Blockage Effects in a Blast Simulator

The confinement of a target by the walls of a blast simulator produces changes in the loading experienced by the target. The changes increase in magnitude with the blockage ratio, the ratio of target area to the simulator cross-sectional area. Computations were made using the HULL hydrocode in an ax...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Ethridge, Noel H, Lottero, Richard E, Wortman, John D, Bertrand, Brian P
Format: Report
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 Ethridge, Noel H
Lottero, Richard E
Wortman, John D
Bertrand, Brian P
description The confinement of a target by the walls of a blast simulator produces changes in the loading experienced by the target. The changes increase in magnitude with the blockage ratio, the ratio of target area to the simulator cross-sectional area. Computations were made using the HULL hydrocode in an axisymmetric configuration for non-decaying waves for different blockage ratios for a cylindrical target. It was found that the flow in the constricted region between the target and the shock tube wall was typically accelerated to velocities greater than the steady flow values behind the incident shock in an unobstructed shock tube. The net axial load on the target computed from the hydrocode results could be related directly to the dynamic pressure in the constricted region, which increased as the blockage was increased. This meant that non-decaying shocks which did not produce net loads sufficient to overturn a target in a shock tube at low blockage could be made to do so by increasing blockage while keeping shock overpressure constant. Thus, tests where the blockage is high can be misleading unless corrections are made for the effect of blockage. The step shock computations provided an extreme case for analysis; similar computations were performed for the other extreme case of a rapidly decaying wave. Although critical flow parameters in the constricted region (e.g. , particle velocity and dynamic pressure) were similarly increased for the decaying wave, the effect on the net force was found to be small. This was because of the overpressure gradient across the target and the reduced importance of drag loading compared to diffraction phase loading.
format Report
fullrecord <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADA143457</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADA143457</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADA1434573</originalsourceid><addsrcrecordid>eNqFybEKwjAQgOEsDqK-gcO9gIO04lxrxM2h7uVILnKY5EpzAR_fDu5OP3z_2jx6SVNVVJaMETB7sJ-JZk6UdYFBq2cqIAEuUdwbXwQ2BHJagDPgolgUBk41osq8NauAsdDu143Z3-yzvx-8shuLciYdu2t3bJv2dG7-7C8RbzOf</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Computational and Experimental Studies of Blockage Effects in a Blast Simulator</title><source>DTIC Technical Reports</source><creator>Ethridge, Noel H ; Lottero, Richard E ; Wortman, John D ; Bertrand, Brian P</creator><creatorcontrib>Ethridge, Noel H ; Lottero, Richard E ; Wortman, John D ; Bertrand, Brian P ; ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD</creatorcontrib><description>The confinement of a target by the walls of a blast simulator produces changes in the loading experienced by the target. The changes increase in magnitude with the blockage ratio, the ratio of target area to the simulator cross-sectional area. Computations were made using the HULL hydrocode in an axisymmetric configuration for non-decaying waves for different blockage ratios for a cylindrical target. It was found that the flow in the constricted region between the target and the shock tube wall was typically accelerated to velocities greater than the steady flow values behind the incident shock in an unobstructed shock tube. The net axial load on the target computed from the hydrocode results could be related directly to the dynamic pressure in the constricted region, which increased as the blockage was increased. This meant that non-decaying shocks which did not produce net loads sufficient to overturn a target in a shock tube at low blockage could be made to do so by increasing blockage while keeping shock overpressure constant. Thus, tests where the blockage is high can be misleading unless corrections are made for the effect of blockage. The step shock computations provided an extreme case for analysis; similar computations were performed for the other extreme case of a rapidly decaying wave. Although critical flow parameters in the constricted region (e.g. , particle velocity and dynamic pressure) were similarly increased for the decaying wave, the effect on the net force was found to be small. This was because of the overpressure gradient across the target and the reduced importance of drag loading compared to diffraction phase loading.</description><language>eng</language><subject>BLAST LOADS ; BLOCKING ; COMPUTERIZED SIMULATION ; DYNAMIC PRESSURE ; EXPLOSION EFFECTS ; Explosions ; FLOW FIELDS ; HULL COMPUTER CODE ; HULL HYDRODYNAMIC CODE ; HYDRODYNAMIC CODES ; NOZZLE THROATS ; ONE DIMENSIONAL FLOW ; OVERPRESSURE ; OVERTURNING ; PE62618A ; SHOCK TUBES ; SHOCK WAVES ; SIMULATORS ; TRUCKS ; WALLS ; WIND TUNNEL TESTS</subject><creationdate>1984</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>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27546,27547</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA143457$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Ethridge, Noel H</creatorcontrib><creatorcontrib>Lottero, Richard E</creatorcontrib><creatorcontrib>Wortman, John D</creatorcontrib><creatorcontrib>Bertrand, Brian P</creatorcontrib><creatorcontrib>ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD</creatorcontrib><title>Computational and Experimental Studies of Blockage Effects in a Blast Simulator</title><description>The confinement of a target by the walls of a blast simulator produces changes in the loading experienced by the target. The changes increase in magnitude with the blockage ratio, the ratio of target area to the simulator cross-sectional area. Computations were made using the HULL hydrocode in an axisymmetric configuration for non-decaying waves for different blockage ratios for a cylindrical target. It was found that the flow in the constricted region between the target and the shock tube wall was typically accelerated to velocities greater than the steady flow values behind the incident shock in an unobstructed shock tube. The net axial load on the target computed from the hydrocode results could be related directly to the dynamic pressure in the constricted region, which increased as the blockage was increased. This meant that non-decaying shocks which did not produce net loads sufficient to overturn a target in a shock tube at low blockage could be made to do so by increasing blockage while keeping shock overpressure constant. Thus, tests where the blockage is high can be misleading unless corrections are made for the effect of blockage. The step shock computations provided an extreme case for analysis; similar computations were performed for the other extreme case of a rapidly decaying wave. Although critical flow parameters in the constricted region (e.g. , particle velocity and dynamic pressure) were similarly increased for the decaying wave, the effect on the net force was found to be small. This was because of the overpressure gradient across the target and the reduced importance of drag loading compared to diffraction phase loading.</description><subject>BLAST LOADS</subject><subject>BLOCKING</subject><subject>COMPUTERIZED SIMULATION</subject><subject>DYNAMIC PRESSURE</subject><subject>EXPLOSION EFFECTS</subject><subject>Explosions</subject><subject>FLOW FIELDS</subject><subject>HULL COMPUTER CODE</subject><subject>HULL HYDRODYNAMIC CODE</subject><subject>HYDRODYNAMIC CODES</subject><subject>NOZZLE THROATS</subject><subject>ONE DIMENSIONAL FLOW</subject><subject>OVERPRESSURE</subject><subject>OVERTURNING</subject><subject>PE62618A</subject><subject>SHOCK TUBES</subject><subject>SHOCK WAVES</subject><subject>SIMULATORS</subject><subject>TRUCKS</subject><subject>WALLS</subject><subject>WIND TUNNEL TESTS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1984</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFybEKwjAQgOEsDqK-gcO9gIO04lxrxM2h7uVILnKY5EpzAR_fDu5OP3z_2jx6SVNVVJaMETB7sJ-JZk6UdYFBq2cqIAEuUdwbXwQ2BHJagDPgolgUBk41osq8NauAsdDu143Z3-yzvx-8shuLciYdu2t3bJv2dG7-7C8RbzOf</recordid><startdate>198406</startdate><enddate>198406</enddate><creator>Ethridge, Noel H</creator><creator>Lottero, Richard E</creator><creator>Wortman, John D</creator><creator>Bertrand, Brian P</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>198406</creationdate><title>Computational and Experimental Studies of Blockage Effects in a Blast Simulator</title><author>Ethridge, Noel H ; Lottero, Richard E ; Wortman, John D ; Bertrand, Brian P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA1434573</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1984</creationdate><topic>BLAST LOADS</topic><topic>BLOCKING</topic><topic>COMPUTERIZED SIMULATION</topic><topic>DYNAMIC PRESSURE</topic><topic>EXPLOSION EFFECTS</topic><topic>Explosions</topic><topic>FLOW FIELDS</topic><topic>HULL COMPUTER CODE</topic><topic>HULL HYDRODYNAMIC CODE</topic><topic>HYDRODYNAMIC CODES</topic><topic>NOZZLE THROATS</topic><topic>ONE DIMENSIONAL FLOW</topic><topic>OVERPRESSURE</topic><topic>OVERTURNING</topic><topic>PE62618A</topic><topic>SHOCK TUBES</topic><topic>SHOCK WAVES</topic><topic>SIMULATORS</topic><topic>TRUCKS</topic><topic>WALLS</topic><topic>WIND TUNNEL TESTS</topic><toplevel>online_resources</toplevel><creatorcontrib>Ethridge, Noel H</creatorcontrib><creatorcontrib>Lottero, Richard E</creatorcontrib><creatorcontrib>Wortman, John D</creatorcontrib><creatorcontrib>Bertrand, Brian P</creatorcontrib><creatorcontrib>ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Ethridge, Noel H</au><au>Lottero, Richard E</au><au>Wortman, John D</au><au>Bertrand, Brian P</au><aucorp>ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Computational and Experimental Studies of Blockage Effects in a Blast Simulator</btitle><date>1984-06</date><risdate>1984</risdate><abstract>The confinement of a target by the walls of a blast simulator produces changes in the loading experienced by the target. The changes increase in magnitude with the blockage ratio, the ratio of target area to the simulator cross-sectional area. Computations were made using the HULL hydrocode in an axisymmetric configuration for non-decaying waves for different blockage ratios for a cylindrical target. It was found that the flow in the constricted region between the target and the shock tube wall was typically accelerated to velocities greater than the steady flow values behind the incident shock in an unobstructed shock tube. The net axial load on the target computed from the hydrocode results could be related directly to the dynamic pressure in the constricted region, which increased as the blockage was increased. This meant that non-decaying shocks which did not produce net loads sufficient to overturn a target in a shock tube at low blockage could be made to do so by increasing blockage while keeping shock overpressure constant. Thus, tests where the blockage is high can be misleading unless corrections are made for the effect of blockage. The step shock computations provided an extreme case for analysis; similar computations were performed for the other extreme case of a rapidly decaying wave. Although critical flow parameters in the constricted region (e.g. , particle velocity and dynamic pressure) were similarly increased for the decaying wave, the effect on the net force was found to be small. This was because of the overpressure gradient across the target and the reduced importance of drag loading compared to diffraction phase loading.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_dtic_stinet_ADA143457
source DTIC Technical Reports
subjects BLAST LOADS
BLOCKING
COMPUTERIZED SIMULATION
DYNAMIC PRESSURE
EXPLOSION EFFECTS
Explosions
FLOW FIELDS
HULL COMPUTER CODE
HULL HYDRODYNAMIC CODE
HYDRODYNAMIC CODES
NOZZLE THROATS
ONE DIMENSIONAL FLOW
OVERPRESSURE
OVERTURNING
PE62618A
SHOCK TUBES
SHOCK WAVES
SIMULATORS
TRUCKS
WALLS
WIND TUNNEL TESTS
title Computational and Experimental Studies of Blockage Effects in a Blast Simulator
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-28T03%3A39%3A03IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-dtic_1RU&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=Computational%20and%20Experimental%20Studies%20of%20Blockage%20Effects%20in%20a%20Blast%20Simulator&rft.au=Ethridge,%20Noel%20H&rft.aucorp=ARMY%20BALLISTIC%20RESEARCH%20LAB%20ABERDEEN%20PROVING%20GROUND%20MD&rft.date=1984-06&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EADA143457%3C/dtic_1RU%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