A hot-film static-pressure probe
The procedure described involves calibrating the probe in the gas of interest over the range of temperatures and pressures anticipated in the wind-tunnel tests and then applying the calibration to reduce the data from those tests. Pressure readings from two probes, one having two hot-film sensors an...
Gespeichert in:
Veröffentlicht in: | AIAA journal 1982-07, Vol.20 (7), p.1022-1023 |
---|---|
Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 1023 |
---|---|
container_issue | 7 |
container_start_page | 1022 |
container_title | AIAA journal |
container_volume | 20 |
creator | Ashby, George C Weinstein, Leonard M |
description | The procedure described involves calibrating the probe in the gas of interest over the range of temperatures and pressures anticipated in the wind-tunnel tests and then applying the calibration to reduce the data from those tests. Pressure readings from two probes, one having two hot-film sensors and an internal sonic orifice and the other connected to a conventional pressure gage, are recorded for several Reynolds numbers and compared. The conventional static-pressure probe with a pair of hot-film sensors and an interior sonic orifice is shown to provide the means of surveying flowfields in hypersonic flow at a rapid rate and with an accuracy of better than + or - 10%. |
doi_str_mv | 10.2514/3.7961 |
format | Article |
fullrecord | <record><control><sourceid>proquest_aiaa_</sourceid><recordid>TN_cdi_proquest_miscellaneous_23419722</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>23419722</sourcerecordid><originalsourceid>FETCH-LOGICAL-a276t-7e720da32062d26679b11d47f984a3e69742c3e6d40f54728819117a2f6bc3013</originalsourceid><addsrcrecordid>eNptkFFLwzAUhYMoOKf-hoIgvmTm3qRJ-ziGU2Hgi4JvIW0T7GjXmqSg_96MDQTx6XA5H-dyDiHXwBaYg7jnC1VKOCEzyDmnvMjfT8mMMQYURI7n5CKEbbpQFTAj2TL7GCJ1bddnIZrY1nT0NoTJ22z0Q2UvyZkzXbBXR52Tt_XD6-qJbl4en1fLDTWoZKTKKmSN4cgkNiilKiuARihXFsJwK0slsE7aCOZyobAooARQBp2sas6Az8ntITd9_ZxsiLpvQ227zuzsMAWNXECpEH_B2g8heOv06Nve-G8NTO8H0FzvB0jg3QE0rTF6O0x-lwocXT02Trup66L9igm9-Q_9E_gDM29jRQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>23419722</pqid></control><display><type>article</type><title>A hot-film static-pressure probe</title><source>Alma/SFX Local Collection</source><creator>Ashby, George C ; Weinstein, Leonard M</creator><creatorcontrib>Ashby, George C ; Weinstein, Leonard M</creatorcontrib><description>The procedure described involves calibrating the probe in the gas of interest over the range of temperatures and pressures anticipated in the wind-tunnel tests and then applying the calibration to reduce the data from those tests. Pressure readings from two probes, one having two hot-film sensors and an internal sonic orifice and the other connected to a conventional pressure gage, are recorded for several Reynolds numbers and compared. The conventional static-pressure probe with a pair of hot-film sensors and an interior sonic orifice is shown to provide the means of surveying flowfields in hypersonic flow at a rapid rate and with an accuracy of better than + or - 10%.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/3.7961</identifier><language>eng</language><ispartof>AIAA journal, 1982-07, Vol.20 (7), p.1022-1023</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Ashby, George C</creatorcontrib><creatorcontrib>Weinstein, Leonard M</creatorcontrib><title>A hot-film static-pressure probe</title><title>AIAA journal</title><description>The procedure described involves calibrating the probe in the gas of interest over the range of temperatures and pressures anticipated in the wind-tunnel tests and then applying the calibration to reduce the data from those tests. Pressure readings from two probes, one having two hot-film sensors and an internal sonic orifice and the other connected to a conventional pressure gage, are recorded for several Reynolds numbers and compared. The conventional static-pressure probe with a pair of hot-film sensors and an interior sonic orifice is shown to provide the means of surveying flowfields in hypersonic flow at a rapid rate and with an accuracy of better than + or - 10%.</description><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1982</creationdate><recordtype>article</recordtype><recordid>eNptkFFLwzAUhYMoOKf-hoIgvmTm3qRJ-ziGU2Hgi4JvIW0T7GjXmqSg_96MDQTx6XA5H-dyDiHXwBaYg7jnC1VKOCEzyDmnvMjfT8mMMQYURI7n5CKEbbpQFTAj2TL7GCJ1bddnIZrY1nT0NoTJ22z0Q2UvyZkzXbBXR52Tt_XD6-qJbl4en1fLDTWoZKTKKmSN4cgkNiilKiuARihXFsJwK0slsE7aCOZyobAooARQBp2sas6Az8ntITd9_ZxsiLpvQ227zuzsMAWNXECpEH_B2g8heOv06Nve-G8NTO8H0FzvB0jg3QE0rTF6O0x-lwocXT02Trup66L9igm9-Q_9E_gDM29jRQ</recordid><startdate>19820701</startdate><enddate>19820701</enddate><creator>Ashby, George C</creator><creator>Weinstein, Leonard M</creator><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>19820701</creationdate><title>A hot-film static-pressure probe</title><author>Ashby, George C ; Weinstein, Leonard M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a276t-7e720da32062d26679b11d47f984a3e69742c3e6d40f54728819117a2f6bc3013</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1982</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ashby, George C</creatorcontrib><creatorcontrib>Weinstein, Leonard M</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ashby, George C</au><au>Weinstein, Leonard M</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A hot-film static-pressure probe</atitle><jtitle>AIAA journal</jtitle><date>1982-07-01</date><risdate>1982</risdate><volume>20</volume><issue>7</issue><spage>1022</spage><epage>1023</epage><pages>1022-1023</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>The procedure described involves calibrating the probe in the gas of interest over the range of temperatures and pressures anticipated in the wind-tunnel tests and then applying the calibration to reduce the data from those tests. Pressure readings from two probes, one having two hot-film sensors and an internal sonic orifice and the other connected to a conventional pressure gage, are recorded for several Reynolds numbers and compared. The conventional static-pressure probe with a pair of hot-film sensors and an interior sonic orifice is shown to provide the means of surveying flowfields in hypersonic flow at a rapid rate and with an accuracy of better than + or - 10%.</abstract><doi>10.2514/3.7961</doi><tpages>2</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0001-1452 |
ispartof | AIAA journal, 1982-07, Vol.20 (7), p.1022-1023 |
issn | 0001-1452 1533-385X |
language | eng |
recordid | cdi_proquest_miscellaneous_23419722 |
source | Alma/SFX Local Collection |
title | A hot-film static-pressure probe |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-19T20%3A13%3A07IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_aiaa_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20hot-film%20static-pressure%20probe&rft.jtitle=AIAA%20journal&rft.au=Ashby,%20George%20C&rft.date=1982-07-01&rft.volume=20&rft.issue=7&rft.spage=1022&rft.epage=1023&rft.pages=1022-1023&rft.issn=0001-1452&rft.eissn=1533-385X&rft_id=info:doi/10.2514/3.7961&rft_dat=%3Cproquest_aiaa_%3E23419722%3C/proquest_aiaa_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=23419722&rft_id=info:pmid/&rfr_iscdi=true |