Special references standard and calibration method for instruments measuring airflow velocity (Discussion)

Abstract A description is given of the draft of a new norm—a method which has been developed for calibrating instruments that measure high subsonic and supersonic airflow velocities and which is based on the use of a special reference standard (SRS) for the Mach-number unit w/a within the range M=0....
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Petunin, A. N. [verfasserIn]

Format:	Artikel
Sprache:	Englisch

Erschienen:	1999

Schlagwörter:	Mach Number Wind Tunnel Control Specimen Velocity Range Absolute Velocity

Anmerkung:	© Kluwer Academic/Plenum Publishers 1999

Übergeordnetes Werk:	Enthalten in: Measurement techniques - Kluwer Academic Publishers-Plenum Publishers, 1958, 42(1999), 3 vom: März, Seite 268-275
Übergeordnetes Werk:	volume:42 ; year:1999 ; number:3 ; month:03 ; pages:268-275

Links:	Volltext

DOI / URN:	10.1007/BF02505151

Katalog-ID:	OLC2047698758

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allfields	10.1007/BF02505151 doi (DE-627)OLC2047698758 (DE-He213)BF02505151-p DE-627 ger DE-627 rakwb eng 620 VZ 11 ssgn Petunin, A. N. verfasserin aut Special references standard and calibration method for instruments measuring airflow velocity (Discussion) 1999 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Kluwer Academic/Plenum Publishers 1999 Abstract A description is given of the draft of a new norm—a method which has been developed for calibrating instruments that measure high subsonic and supersonic airflow velocities and which is based on the use of a special reference standard (SRS) for the Mach-number unit w/a within the range M=0.3–4.0 (where w is absolute velocity and a is sonic velocity). The reference standard reproduces the Mach-number unit with a standard deviation no greater that the deviation obtained from ten independent measurements $ S_{M} $=0.002–0.0002 M, which is equivalent to an error of absolute velocity $ S_{w} $=(0.002a–0.0002w) m/sec. Here, a is sonic velocity at the temperature of the flow. Working standards and control specimens are also examined. The errors made in their comparisons with the SRS and working instruments are stipulated along with the ranges of the allowable absolute errors of the working instruments. Mach Number Wind Tunnel Control Specimen Velocity Range Absolute Velocity Enthalten in Measurement techniques Kluwer Academic Publishers-Plenum Publishers, 1958 42(1999), 3 vom: März, Seite 268-275 (DE-627)129596876 (DE-600)240846-6 (DE-576)015090051 0543-1972 nnns volume:42 year:1999 number:3 month:03 pages:268-275 https://doi.org/10.1007/BF02505151 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_40 GBV_ILN_70 GBV_ILN_170 GBV_ILN_2015 AR 42 1999 3 03 268-275
spelling	10.1007/BF02505151 doi (DE-627)OLC2047698758 (DE-He213)BF02505151-p DE-627 ger DE-627 rakwb eng 620 VZ 11 ssgn Petunin, A. N. verfasserin aut Special references standard and calibration method for instruments measuring airflow velocity (Discussion) 1999 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Kluwer Academic/Plenum Publishers 1999 Abstract A description is given of the draft of a new norm—a method which has been developed for calibrating instruments that measure high subsonic and supersonic airflow velocities and which is based on the use of a special reference standard (SRS) for the Mach-number unit w/a within the range M=0.3–4.0 (where w is absolute velocity and a is sonic velocity). The reference standard reproduces the Mach-number unit with a standard deviation no greater that the deviation obtained from ten independent measurements $ S_{M} $=0.002–0.0002 M, which is equivalent to an error of absolute velocity $ S_{w} $=(0.002a–0.0002w) m/sec. Here, a is sonic velocity at the temperature of the flow. Working standards and control specimens are also examined. The errors made in their comparisons with the SRS and working instruments are stipulated along with the ranges of the allowable absolute errors of the working instruments. Mach Number Wind Tunnel Control Specimen Velocity Range Absolute Velocity Enthalten in Measurement techniques Kluwer Academic Publishers-Plenum Publishers, 1958 42(1999), 3 vom: März, Seite 268-275 (DE-627)129596876 (DE-600)240846-6 (DE-576)015090051 0543-1972 nnns volume:42 year:1999 number:3 month:03 pages:268-275 https://doi.org/10.1007/BF02505151 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_40 GBV_ILN_70 GBV_ILN_170 GBV_ILN_2015 AR 42 1999 3 03 268-275
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title_sort	special references standard and calibration method for instruments measuring airflow velocity (discussion)
title_auth	Special references standard and calibration method for instruments measuring airflow velocity (Discussion)
abstract	Abstract A description is given of the draft of a new norm—a method which has been developed for calibrating instruments that measure high subsonic and supersonic airflow velocities and which is based on the use of a special reference standard (SRS) for the Mach-number unit w/a within the range M=0.3–4.0 (where w is absolute velocity and a is sonic velocity). The reference standard reproduces the Mach-number unit with a standard deviation no greater that the deviation obtained from ten independent measurements $ S_{M} $=0.002–0.0002 M, which is equivalent to an error of absolute velocity $ S_{w} $=(0.002a–0.0002w) m/sec. Here, a is sonic velocity at the temperature of the flow. Working standards and control specimens are also examined. The errors made in their comparisons with the SRS and working instruments are stipulated along with the ranges of the allowable absolute errors of the working instruments. © Kluwer Academic/Plenum Publishers 1999
abstractGer	Abstract A description is given of the draft of a new norm—a method which has been developed for calibrating instruments that measure high subsonic and supersonic airflow velocities and which is based on the use of a special reference standard (SRS) for the Mach-number unit w/a within the range M=0.3–4.0 (where w is absolute velocity and a is sonic velocity). The reference standard reproduces the Mach-number unit with a standard deviation no greater that the deviation obtained from ten independent measurements $ S_{M} $=0.002–0.0002 M, which is equivalent to an error of absolute velocity $ S_{w} $=(0.002a–0.0002w) m/sec. Here, a is sonic velocity at the temperature of the flow. Working standards and control specimens are also examined. The errors made in their comparisons with the SRS and working instruments are stipulated along with the ranges of the allowable absolute errors of the working instruments. © Kluwer Academic/Plenum Publishers 1999
abstract_unstemmed	Abstract A description is given of the draft of a new norm—a method which has been developed for calibrating instruments that measure high subsonic and supersonic airflow velocities and which is based on the use of a special reference standard (SRS) for the Mach-number unit w/a within the range M=0.3–4.0 (where w is absolute velocity and a is sonic velocity). The reference standard reproduces the Mach-number unit with a standard deviation no greater that the deviation obtained from ten independent measurements $ S_{M} $=0.002–0.0002 M, which is equivalent to an error of absolute velocity $ S_{w} $=(0.002a–0.0002w) m/sec. Here, a is sonic velocity at the temperature of the flow. Working standards and control specimens are also examined. The errors made in their comparisons with the SRS and working instruments are stipulated along with the ranges of the allowable absolute errors of the working instruments. © Kluwer Academic/Plenum Publishers 1999
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title_short	Special references standard and calibration method for instruments measuring airflow velocity (Discussion)
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N.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Special references standard and calibration method for instruments measuring airflow velocity (Discussion)</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">1999</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Kluwer Academic/Plenum Publishers 1999</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract A description is given of the draft of a new norm—a method which has been developed for calibrating instruments that measure high subsonic and supersonic airflow velocities and which is based on the use of a special reference standard (SRS) for the Mach-number unit w/a within the range M=0.3–4.0 (where w is absolute velocity and a is sonic velocity). The reference standard reproduces the Mach-number unit with a standard deviation no greater that the deviation obtained from ten independent measurements $ S_{M} $=0.002–0.0002 M, which is equivalent to an error of absolute velocity $ S_{w} $=(0.002a–0.0002w) m/sec. Here, a is sonic velocity at the temperature of the flow. Working standards and control specimens are also examined. The errors made in their comparisons with the SRS and working instruments are stipulated along with the ranges of the allowable absolute errors of the working instruments.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Mach Number</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Wind Tunnel</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Control Specimen</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Velocity Range</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Absolute Velocity</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Measurement techniques</subfield><subfield code="d">Kluwer Academic Publishers-Plenum Publishers, 1958</subfield><subfield code="g">42(1999), 3 vom: März, Seite 268-275</subfield><subfield code="w">(DE-627)129596876</subfield><subfield code="w">(DE-600)240846-6</subfield><subfield code="w">(DE-576)015090051</subfield><subfield code="x">0543-1972</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:42</subfield><subfield code="g">year:1999</subfield><subfield code="g">number:3</subfield><subfield code="g">month:03</subfield><subfield code="g">pages:268-275</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1007/BF02505151</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_OLC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-TEC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-PHY</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_170</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2015</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">42</subfield><subfield code="j">1999</subfield><subfield code="e">3</subfield><subfield code="c">03</subfield><subfield code="h">268-275</subfield></datafield></record></collection>
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