20.500.12556/RUL-170498 Method for correction of the systematic errors in detected shock wave passage times in the shock tube 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. diaphragmless shock tubes time-varying pressure time-of-flight method dynamic response correction brezmembranske udarne cevi časovno spreminjajoči tlak metoda časa preleta dinamični odziv korekcija true false false Angleški jezik Slovenski jezik Članek v reviji 2025-07-07 11:54:47 2025-07-07 11:54:51 2025-07-08 04:20:22 0000-00-00 00:00:00 2022 0 0 Str. 1-5 0000-00-00 Zaloznikova Objavljeno NiDoloceno 0000-00-00 0000-00-00 0000-00-00 531.7 140261379 140258051 RAZ_Hernandez_Castro_Francisco_Javier_2022.pdf RAZ_Hernandez_Castro_Francisco_Javier_2022.pdf 1 F5A877249808D4553C59AB4C38EC7026 efe618aa9eeb977bd8e4290c5e19c6a1722dc7f56280bbb8c465bcc7004f76a2 84a6e6a5-5b16-11f0-b232-0050569b8976 https://repozitorij.uni-lj.si/Dokument.php?lang=slv&id=212509 Fakulteta za strojništvo 0 0 0