In-tube shock wave compression by piston effect of unsteady jet

A high-pressure field is generated in a circular tube by introducing an unsteady jet from its open end. The head of this jet acts as a piston, driving compression waves ahead of it. The peak value of the induced overpressure is evaluated as a solution of a Riemann problem, wherein the jet head is eq...

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Main Authors: Daisuke KUWABARA, Hirokatsu KAWASAKI, Akira IWAKAWA, Akihiro SASOH, Tetsuya YAMASHITA, Koji TAGUCHI
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2020-04-01
Series:Mechanical Engineering Journal
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/mej/7/3/7_19-00534/_pdf/-char/en
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author Daisuke KUWABARA
Hirokatsu KAWASAKI
Akira IWAKAWA
Akihiro SASOH
Tetsuya YAMASHITA
Koji TAGUCHI
author_facet Daisuke KUWABARA
Hirokatsu KAWASAKI
Akira IWAKAWA
Akihiro SASOH
Tetsuya YAMASHITA
Koji TAGUCHI
author_sort Daisuke KUWABARA
collection DOAJ
description A high-pressure field is generated in a circular tube by introducing an unsteady jet from its open end. The head of this jet acts as a piston, driving compression waves ahead of it. The peak value of the induced overpressure is evaluated as a solution of a Riemann problem, wherein the jet head is equivalent to a piston head. The jet head of the driver gas, with a filling pressure of 400 kPa, is equivalent to a piston head moving at 160 m/s. This high-pressure generation scheme through the “piston effect” is useful for industrial applications, including filter cleaning in dust collectors, and as an interesting example of unsteady, compressible fluid dynamics.
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spelling doaj.art-89a32f223dca4515a6e93bcf25140b932022-12-21T19:25:42ZengThe Japan Society of Mechanical EngineersMechanical Engineering Journal2187-97452020-04-017319-0053419-0053410.1299/mej.19-00534mejIn-tube shock wave compression by piston effect of unsteady jetDaisuke KUWABARA0Hirokatsu KAWASAKI1Akira IWAKAWA2Akihiro SASOH3Tetsuya YAMASHITA4Koji TAGUCHI5Department of Aerospace Engineering, Nagoya UniversityDepartment of Aerospace Engineering, Nagoya UniversityDepartment of Aerospace Engineering, Nagoya UniversityDepartment of Aerospace Engineering, Nagoya UniversityUS URASAKI Co., LtdUS URASAKI Co., LtdA high-pressure field is generated in a circular tube by introducing an unsteady jet from its open end. The head of this jet acts as a piston, driving compression waves ahead of it. The peak value of the induced overpressure is evaluated as a solution of a Riemann problem, wherein the jet head is equivalent to a piston head. The jet head of the driver gas, with a filling pressure of 400 kPa, is equivalent to a piston head moving at 160 m/s. This high-pressure generation scheme through the “piston effect” is useful for industrial applications, including filter cleaning in dust collectors, and as an interesting example of unsteady, compressible fluid dynamics.https://www.jstage.jst.go.jp/article/mej/7/3/7_19-00534/_pdf/-char/encompressible fluid dynamicsshock waveunsteady jetin-tube compression
spellingShingle Daisuke KUWABARA
Hirokatsu KAWASAKI
Akira IWAKAWA
Akihiro SASOH
Tetsuya YAMASHITA
Koji TAGUCHI
In-tube shock wave compression by piston effect of unsteady jet
Mechanical Engineering Journal
compressible fluid dynamics
shock wave
unsteady jet
in-tube compression
title In-tube shock wave compression by piston effect of unsteady jet
title_full In-tube shock wave compression by piston effect of unsteady jet
title_fullStr In-tube shock wave compression by piston effect of unsteady jet
title_full_unstemmed In-tube shock wave compression by piston effect of unsteady jet
title_short In-tube shock wave compression by piston effect of unsteady jet
title_sort in tube shock wave compression by piston effect of unsteady jet
topic compressible fluid dynamics
shock wave
unsteady jet
in-tube compression
url https://www.jstage.jst.go.jp/article/mej/7/3/7_19-00534/_pdf/-char/en
work_keys_str_mv AT daisukekuwabara intubeshockwavecompressionbypistoneffectofunsteadyjet
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AT akiraiwakawa intubeshockwavecompressionbypistoneffectofunsteadyjet
AT akihirosasoh intubeshockwavecompressionbypistoneffectofunsteadyjet
AT tetsuyayamashita intubeshockwavecompressionbypistoneffectofunsteadyjet
AT kojitaguchi intubeshockwavecompressionbypistoneffectofunsteadyjet