The Space Shuttle liftoff pressure wave
The pressure wave produced during the launch of the Space Shuttle and its dynamic effects on ground support structures are studied in this paper. The discrete form of the Fourier transform and the fast Fourier transform algorithm are employed to characterize the pressure wave and to generate design...
Gespeichert in:
Veröffentlicht in: | Computers & structures 1996-05, Vol.59 (4), p.783-787 |
---|---|
Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 787 |
---|---|
container_issue | 4 |
container_start_page | 783 |
container_title | Computers & structures |
container_volume | 59 |
creator | Willis, S.L. Carroll, W.F. Yang, Tyng-Lin |
description | The pressure wave produced during the launch of the Space Shuttle and its dynamic effects on ground support structures are studied in this paper. The discrete form of the Fourier transform and the fast Fourier transform algorithm are employed to characterize the pressure wave and to generate design and evaluation data. Analysis is performed on pressure recordings collected from eight pressure transducers mounted on the roof and walls of a building approximately 90 m West of Launch Pad 39A at the Kennedy Space Center. A total of 23 pressure pulses were sampled every 0.25 ms for a 10s duration from six different launches. The analysis produces a pressure-time plot and power spectrum, representing the frequency content of the pressure wave which identifies its ability to excite a structure. Also produced are response spectra for each pressure wave for various amounts of damping. These spectra may be used to predict the dynamic response of a structure located near a launch site. |
doi_str_mv | 10.1016/0045-7949(95)00282-0 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_26354022</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>0045794995002820</els_id><sourcerecordid>26354022</sourcerecordid><originalsourceid>FETCH-LOGICAL-c364t-4e114d1d1b158bcd3b250100030dceddc438f52e6af5c23e556ed94a21f9ffad3</originalsourceid><addsrcrecordid>eNp9kEtPwzAQhC0EEqXwDzjkgHgcAutnkwsSqnhJlThQzpZrr1WjtAl2UsS_J6FVj1x2L9_MaIaQcwq3FKi6AxAyn5SivC7lDQArWA4HZESLSZkzJvghGe2RY3KS0icAKAEwIlfzJWbvjbH9XXZtW2FWBd_W3mdNxJS6iNm32eApOfKmSni2-2Py8fQ4n77ks7fn1-nDLLdciTYXSKlw1NEFlcXCOr5gEmifxsFZdM4KXnjJUBkvLeMopUJXCsOoL703jo_J5da3ifVXh6nVq5AsVpVZY90lzRSXAhjrQbEFbaxTiuh1E8PKxB9NQQ-r6KGyHirrUuq_VTT0soudv0nWVD6atQ1pr-VAhZoM2P0Ww77rJmDUyQZc9xVCRNtqV4f_c34Bts90iw</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>26354022</pqid></control><display><type>article</type><title>The Space Shuttle liftoff pressure wave</title><source>Access via ScienceDirect (Elsevier)</source><creator>Willis, S.L. ; Carroll, W.F. ; Yang, Tyng-Lin</creator><creatorcontrib>Willis, S.L. ; Carroll, W.F. ; Yang, Tyng-Lin</creatorcontrib><description>The pressure wave produced during the launch of the Space Shuttle and its dynamic effects on ground support structures are studied in this paper. The discrete form of the Fourier transform and the fast Fourier transform algorithm are employed to characterize the pressure wave and to generate design and evaluation data. Analysis is performed on pressure recordings collected from eight pressure transducers mounted on the roof and walls of a building approximately 90 m West of Launch Pad 39A at the Kennedy Space Center. A total of 23 pressure pulses were sampled every 0.25 ms for a 10s duration from six different launches. The analysis produces a pressure-time plot and power spectrum, representing the frequency content of the pressure wave which identifies its ability to excite a structure. Also produced are response spectra for each pressure wave for various amounts of damping. These spectra may be used to predict the dynamic response of a structure located near a launch site.</description><identifier>ISSN: 0045-7949</identifier><identifier>EISSN: 1879-2243</identifier><identifier>DOI: 10.1016/0045-7949(95)00282-0</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Applied sciences ; Exact sciences and technology ; Ground, air and sea transportation, marine construction ; Miscellaneous transportation</subject><ispartof>Computers & structures, 1996-05, Vol.59 (4), p.783-787</ispartof><rights>1996</rights><rights>1996 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c364t-4e114d1d1b158bcd3b250100030dceddc438f52e6af5c23e556ed94a21f9ffad3</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/0045-7949(95)00282-0$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>315,781,785,3551,27928,27929,45999</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=3014670$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Willis, S.L.</creatorcontrib><creatorcontrib>Carroll, W.F.</creatorcontrib><creatorcontrib>Yang, Tyng-Lin</creatorcontrib><title>The Space Shuttle liftoff pressure wave</title><title>Computers & structures</title><description>The pressure wave produced during the launch of the Space Shuttle and its dynamic effects on ground support structures are studied in this paper. The discrete form of the Fourier transform and the fast Fourier transform algorithm are employed to characterize the pressure wave and to generate design and evaluation data. Analysis is performed on pressure recordings collected from eight pressure transducers mounted on the roof and walls of a building approximately 90 m West of Launch Pad 39A at the Kennedy Space Center. A total of 23 pressure pulses were sampled every 0.25 ms for a 10s duration from six different launches. The analysis produces a pressure-time plot and power spectrum, representing the frequency content of the pressure wave which identifies its ability to excite a structure. Also produced are response spectra for each pressure wave for various amounts of damping. These spectra may be used to predict the dynamic response of a structure located near a launch site.</description><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Ground, air and sea transportation, marine construction</subject><subject>Miscellaneous transportation</subject><issn>0045-7949</issn><issn>1879-2243</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1996</creationdate><recordtype>article</recordtype><recordid>eNp9kEtPwzAQhC0EEqXwDzjkgHgcAutnkwsSqnhJlThQzpZrr1WjtAl2UsS_J6FVj1x2L9_MaIaQcwq3FKi6AxAyn5SivC7lDQArWA4HZESLSZkzJvghGe2RY3KS0icAKAEwIlfzJWbvjbH9XXZtW2FWBd_W3mdNxJS6iNm32eApOfKmSni2-2Py8fQ4n77ks7fn1-nDLLdciTYXSKlw1NEFlcXCOr5gEmifxsFZdM4KXnjJUBkvLeMopUJXCsOoL703jo_J5da3ifVXh6nVq5AsVpVZY90lzRSXAhjrQbEFbaxTiuh1E8PKxB9NQQ-r6KGyHirrUuq_VTT0soudv0nWVD6atQ1pr-VAhZoM2P0Ww77rJmDUyQZc9xVCRNtqV4f_c34Bts90iw</recordid><startdate>19960517</startdate><enddate>19960517</enddate><creator>Willis, S.L.</creator><creator>Carroll, W.F.</creator><creator>Yang, Tyng-Lin</creator><general>Elsevier Ltd</general><general>Elsevier Science</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>8FD</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope></search><sort><creationdate>19960517</creationdate><title>The Space Shuttle liftoff pressure wave</title><author>Willis, S.L. ; Carroll, W.F. ; Yang, Tyng-Lin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c364t-4e114d1d1b158bcd3b250100030dceddc438f52e6af5c23e556ed94a21f9ffad3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1996</creationdate><topic>Applied sciences</topic><topic>Exact sciences and technology</topic><topic>Ground, air and sea transportation, marine construction</topic><topic>Miscellaneous transportation</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Willis, S.L.</creatorcontrib><creatorcontrib>Carroll, W.F.</creatorcontrib><creatorcontrib>Yang, Tyng-Lin</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Computers & structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Willis, S.L.</au><au>Carroll, W.F.</au><au>Yang, Tyng-Lin</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>The Space Shuttle liftoff pressure wave</atitle><jtitle>Computers & structures</jtitle><date>1996-05-17</date><risdate>1996</risdate><volume>59</volume><issue>4</issue><spage>783</spage><epage>787</epage><pages>783-787</pages><issn>0045-7949</issn><eissn>1879-2243</eissn><abstract>The pressure wave produced during the launch of the Space Shuttle and its dynamic effects on ground support structures are studied in this paper. The discrete form of the Fourier transform and the fast Fourier transform algorithm are employed to characterize the pressure wave and to generate design and evaluation data. Analysis is performed on pressure recordings collected from eight pressure transducers mounted on the roof and walls of a building approximately 90 m West of Launch Pad 39A at the Kennedy Space Center. A total of 23 pressure pulses were sampled every 0.25 ms for a 10s duration from six different launches. The analysis produces a pressure-time plot and power spectrum, representing the frequency content of the pressure wave which identifies its ability to excite a structure. Also produced are response spectra for each pressure wave for various amounts of damping. These spectra may be used to predict the dynamic response of a structure located near a launch site.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/0045-7949(95)00282-0</doi><tpages>5</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0045-7949 |
ispartof | Computers & structures, 1996-05, Vol.59 (4), p.783-787 |
issn | 0045-7949 1879-2243 |
language | eng |
recordid | cdi_proquest_miscellaneous_26354022 |
source | Access via ScienceDirect (Elsevier) |
subjects | Applied sciences Exact sciences and technology Ground, air and sea transportation, marine construction Miscellaneous transportation |
title | The Space Shuttle liftoff pressure wave |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-17T12%3A08%3A55IST&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=The%20Space%20Shuttle%20liftoff%20pressure%20wave&rft.jtitle=Computers%20&%20structures&rft.au=Willis,%20S.L.&rft.date=1996-05-17&rft.volume=59&rft.issue=4&rft.spage=783&rft.epage=787&rft.pages=783-787&rft.issn=0045-7949&rft.eissn=1879-2243&rft_id=info:doi/10.1016/0045-7949(95)00282-0&rft_dat=%3Cproquest_cross%3E26354022%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=26354022&rft_id=info:pmid/&rft_els_id=0045794995002820&rfr_iscdi=true |