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Cryogenic Pressure Surge Data Set: PS-LN2-Set1

Klein, Sebastian and Traudt, Tobias and Deeken, Jan C. (2025) Cryogenic Pressure Surge Data Set: PS-LN2-Set1. [Other]

Full text not available from this repository.

Official URL: https://zenodo.org/records/15526459

Abstract

Cryogenic fluid hammer experiments have been performed at the Fluid Transient Fest Facility (FTTF) at the Institute of Space Propulsion of the German Aerospace Center (DLR) in Lampoldshausen.

A pressure surge is created by using a fast closing valve to stop a stationary flow of liquid nitrogen in a pipeline. The pressure wave is then travelling back and forth between the valve and a reservoir upstream of the pipe. Due to the high amplitude of this pressure wave, the pressure drops below the vapor pressure, causing cavitation near the valve.

The dataset includes 9 test cases across a wide range of pressure and flow velocity. At maximum, a flow velocity of 13 m/s results in a pressure surge amplitude exceeding 100 bar. It also features high-frequency pressure sensors, providing detailed insights into the phenomenon.

Item URL in elib:https://elib.dlr.de/214268/
Document Type:Other
Title:Cryogenic Pressure Surge Data Set: PS-LN2-Set1
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Klein, SebastianSebastian.Klein (at) dlr.dehttps://orcid.org/0000-0002-0579-655XUNSPECIFIED
Traudt, TobiasTobias.Traudt (at) dlr.dehttps://orcid.org/0000-0002-0206-0483186785068
Deeken, Jan C.Jan.Deeken (at) dlr.dehttps://orcid.org/0000-0002-5714-8845UNSPECIFIED
Date:22 May 2025
Refereed publication:No
Open Access:No
Status:Published
Keywords:fluid hammer, cavitation, pressure surge, liquid nitrogen, rocket engine, feed line system, fluid transients
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Lead Project - Upper Level Research Network
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Engine Systems
Deposited By: Hanke, Michaela
Deposited On:27 Jun 2025 11:39
Last Modified:27 Jun 2025 11:39

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