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<metadata xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:dc="http://purl.org/dc/elements/1.1/"><dc:title>Method for correction of the systematic errors in detected shock wave passage times in the shock tube</dc:title><dc:creator>Hernández Castro,	Francisco Javier	(Avtor)
	</dc:creator><dc:creator>Svete,	Andrej	(Avtor)
	</dc:creator><dc:creator>Kutin,	Jože	(Avtor)
	</dc:creator><dc:subject>diaphragmless shock tubes</dc:subject><dc:subject>time-varying pressure</dc:subject><dc:subject>time-of-flight method</dc:subject><dc:subject>dynamic response</dc:subject><dc:subject>correction</dc:subject><dc:description>The most important uncertainty component of the pressure step signal determined at the end-wall of the shock tube is associated with the uncertainties of the shock wave velocity and the arrival time of the shock front. Both are determined using a time-of-flight method and are therefore greatly affected by the errors in the detected times of the shock wave passages over the side-wall pressure sensors installed along the shock tube. This paper introduces a method for an automated correction of the systematic errors due to non-ideal dynamic response of the side-wall pressure sensors.</dc:description><dc:date>2022</dc:date><dc:date>2025-07-07 11:54:47</dc:date><dc:type>Članek v reviji</dc:type><dc:identifier>170498</dc:identifier><dc:identifier>UDK: 531.7</dc:identifier><dc:identifier>COBISS_ID: 140261379</dc:identifier><dc:identifier>OceCobissID: 140258051</dc:identifier><dc:language>sl</dc:language></metadata>
