Quantification of Residual Stress from Photonic Signatures of Fused Silica

A commercially available grey-field polariscope (GFP) instrument for photoelastic examination is used to assess impact damage inflicted upon the outer-most pane of Space Shuttle windows made from fused silica. A method and apparatus for calibration of the stress-optic coefficient using four-point be...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Cramer, K. Elliott, Hayward, Maurice, Yost, William E.
Format: Tagungsbericht
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 Cramer, K. Elliott
Hayward, Maurice
Yost, William E.
description A commercially available grey-field polariscope (GFP) instrument for photoelastic examination is used to assess impact damage inflicted upon the outer-most pane of Space Shuttle windows made from fused silica. A method and apparatus for calibration of the stress-optic coefficient using four-point bending is discussed. The results are validated on known material (acrylic) and are found to agree with literature values to within 6%. The calibration procedure is then applied to fused-silica specimens and the stress-optic coefficient is determined to be 2.43 +/- 0.54 x 10(exp -12)/Pa. Fused silica specimens containing impacts artificially made at NASA's Hypervelocity Impact Technology Facility (HIT-F), to simulate damage typical during space flight, are examined. The damage sites are cored from fused silica window carcasses and examined with the GFP. The calibrated GFP measurements of residual stress patterns surrounding the damage sites are presented. Keywords: Glass, fused silica, photoelasticity, residual stress
format Conference Proceeding
fullrecord <record><control><sourceid>nasa_CYI</sourceid><recordid>TN_cdi_nasa_ntrs_20160005098</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>20160005098</sourcerecordid><originalsourceid>FETCH-nasa_ntrs_201600050983</originalsourceid><addsrcrecordid>eNrjZPAKLE3MK8lMy0xOLMnMz1PIT1MISi3OTClNzFEILilKLS5WSCvKz1UIyMgvyc_LTFYIzkzPSywpBcqA1LqVFqemAMVygPp5GFjTEnOKU3mhNDeDjJtriLOHbl5icWJ8XklRcbyRgaGZgYGBqYGlhTEBaQDsKDDM</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Quantification of Residual Stress from Photonic Signatures of Fused Silica</title><source>NASA Technical Reports Server</source><creator>Cramer, K. Elliott ; Hayward, Maurice ; Yost, William E.</creator><creatorcontrib>Cramer, K. Elliott ; Hayward, Maurice ; Yost, William E.</creatorcontrib><description>A commercially available grey-field polariscope (GFP) instrument for photoelastic examination is used to assess impact damage inflicted upon the outer-most pane of Space Shuttle windows made from fused silica. A method and apparatus for calibration of the stress-optic coefficient using four-point bending is discussed. The results are validated on known material (acrylic) and are found to agree with literature values to within 6%. The calibration procedure is then applied to fused-silica specimens and the stress-optic coefficient is determined to be 2.43 +/- 0.54 x 10(exp -12)/Pa. Fused silica specimens containing impacts artificially made at NASA's Hypervelocity Impact Technology Facility (HIT-F), to simulate damage typical during space flight, are examined. The damage sites are cored from fused silica window carcasses and examined with the GFP. The calibrated GFP measurements of residual stress patterns surrounding the damage sites are presented. Keywords: Glass, fused silica, photoelasticity, residual stress</description><language>eng</language><publisher>Langley Research Center</publisher><subject>Optics</subject><creationdate>2013</creationdate><rights>Copyright Determination: PUBLIC_USE_PERMITTED</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,776,796</link.rule.ids><linktorsrc>$$Uhttps://ntrs.nasa.gov/citations/20160005098$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Cramer, K. Elliott</creatorcontrib><creatorcontrib>Hayward, Maurice</creatorcontrib><creatorcontrib>Yost, William E.</creatorcontrib><title>Quantification of Residual Stress from Photonic Signatures of Fused Silica</title><description>A commercially available grey-field polariscope (GFP) instrument for photoelastic examination is used to assess impact damage inflicted upon the outer-most pane of Space Shuttle windows made from fused silica. A method and apparatus for calibration of the stress-optic coefficient using four-point bending is discussed. The results are validated on known material (acrylic) and are found to agree with literature values to within 6%. The calibration procedure is then applied to fused-silica specimens and the stress-optic coefficient is determined to be 2.43 +/- 0.54 x 10(exp -12)/Pa. Fused silica specimens containing impacts artificially made at NASA's Hypervelocity Impact Technology Facility (HIT-F), to simulate damage typical during space flight, are examined. The damage sites are cored from fused silica window carcasses and examined with the GFP. The calibrated GFP measurements of residual stress patterns surrounding the damage sites are presented. Keywords: Glass, fused silica, photoelasticity, residual stress</description><subject>Optics</subject><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2013</creationdate><recordtype>conference_proceeding</recordtype><sourceid>CYI</sourceid><recordid>eNrjZPAKLE3MK8lMy0xOLMnMz1PIT1MISi3OTClNzFEILilKLS5WSCvKz1UIyMgvyc_LTFYIzkzPSywpBcqA1LqVFqemAMVygPp5GFjTEnOKU3mhNDeDjJtriLOHbl5icWJ8XklRcbyRgaGZgYGBqYGlhTEBaQDsKDDM</recordid><startdate>20130721</startdate><enddate>20130721</enddate><creator>Cramer, K. Elliott</creator><creator>Hayward, Maurice</creator><creator>Yost, William E.</creator><scope>CYE</scope><scope>CYI</scope></search><sort><creationdate>20130721</creationdate><title>Quantification of Residual Stress from Photonic Signatures of Fused Silica</title><author>Cramer, K. Elliott ; Hayward, Maurice ; Yost, William E.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_201600050983</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Optics</topic><toplevel>online_resources</toplevel><creatorcontrib>Cramer, K. Elliott</creatorcontrib><creatorcontrib>Hayward, Maurice</creatorcontrib><creatorcontrib>Yost, William E.</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Cramer, K. Elliott</au><au>Hayward, Maurice</au><au>Yost, William E.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Quantification of Residual Stress from Photonic Signatures of Fused Silica</atitle><date>2013-07-21</date><risdate>2013</risdate><abstract>A commercially available grey-field polariscope (GFP) instrument for photoelastic examination is used to assess impact damage inflicted upon the outer-most pane of Space Shuttle windows made from fused silica. A method and apparatus for calibration of the stress-optic coefficient using four-point bending is discussed. The results are validated on known material (acrylic) and are found to agree with literature values to within 6%. The calibration procedure is then applied to fused-silica specimens and the stress-optic coefficient is determined to be 2.43 +/- 0.54 x 10(exp -12)/Pa. Fused silica specimens containing impacts artificially made at NASA's Hypervelocity Impact Technology Facility (HIT-F), to simulate damage typical during space flight, are examined. The damage sites are cored from fused silica window carcasses and examined with the GFP. The calibrated GFP measurements of residual stress patterns surrounding the damage sites are presented. Keywords: Glass, fused silica, photoelasticity, residual stress</abstract><cop>Langley Research Center</cop><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_nasa_ntrs_20160005098
source NASA Technical Reports Server
subjects Optics
title Quantification of Residual Stress from Photonic Signatures of Fused Silica
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-12T12%3A02%3A49IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-nasa_CYI&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Quantification%20of%20Residual%20Stress%20from%20Photonic%20Signatures%20of%20Fused%20Silica&rft.au=Cramer,%20K.%20Elliott&rft.date=2013-07-21&rft_id=info:doi/&rft_dat=%3Cnasa_CYI%3E20160005098%3C/nasa_CYI%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