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In industrial applications, the effects of explosions must be considered as important part of safety assessments. This is particularly crucial in applications involving explosives or pressurized containers. The evaluation of the effects of shock waves on the environment becomes essential in such scenarios and requires comprehensive experimental test series.
This article therefore presents a test bench that can generate and record reproducible, adjustable shock waves with short set-up times. The presented data proves the quality and validity of this set-up to generate case relevant data, like overpressure in comparison to explosives and shock tubes, with load cases of high relevance.
The presented free-field tests are carried out at BAM's Test Site Technical Safety (TTS) with a gas-operated shock wave generator. This shock wave generator consists of a pressure vessel (autoclave) that is operated with a detonable gas mixture or compressed air. The pressure is released through an orifice by the instantaneous bursting of a diaphragm.
The aim is to develop further the novel test bench that generates shock waves on models in a generic scenario and offers several advantages to create a valid database for the effects of shock waves.
In contrast to classic shock tubes, this test bench offers the advantage of realistic hemispherical shock wave propagation and scalability, both for the investigated model size and for the generation of load cases, so that different model variables can be investigated under different boundary conditions (mainly overpressure); at the same time, typical interference of a shock tube experiment due to reflections, blockage effects and the following fluid flow can be minimized. These negative influences are not realistic compared to the ideal event of a detonation.
A test setup was developed at the BAM test site to generate and record reproducible, adjustable shock waves resulting from gas detonations. The setup is used to study the impact of blasts on humans and structures with short setup times. To further develop this innovative test bench and improve reproducibility, the ignition source and gas composition is analysed in more detail.
The experimental setup consists of a cylindrical pressure vessel (autoclave) that is operated with acetylene and oxygen at ambient pressure. The elevated pressure resulting from the combustion process is released through an orifice by the instantaneous rupture of a diaphragm. The shock propagates symmetrically into the free field, where it interacts with the models and sensors to be analysed. With this design, shock waves with a typical ideal Friedlander waveform characteristic, except for a reflection and a muzzle blast-like behavior that deviates from the ideal characteristics, can be generated. This setup enables an average peak overpressure of 88 kPa. By using exploding wires as an ignition source in comparison to a fusehead, the reproducibility was significantly increased during the test to
σ=2.8 kPa from σ=9.5 kPa previously.
The presented data confirms the quality and reliability of this setup in generating realistic, reproducible shocks.
A simple test bench was set up on the BAM test site to
investigate shock waves caused by gas detonations. The aim was to build
a simple mobile test bench that can be used for various applications, to
demonstrate the vaildity and for comparison with other test benches. For
this purpose a balloon filled with acetylene and oxygen at atmospheric
pressure with an electric ignitor was used. The characteristics of the
shock waves can be scaled via the gaseous mixture, the filling quantity
of the balloon and the distance to the sensors. Pressure sensors were
set up around the balloon at various distances to measure the shock.
With the help of the high-speed recordings and the Rankine Hugoniot
equations, the shock front pressure was estimated and compared with
the results of the pressure sensors. In order to validate the results of
this test bench, they were compared with an experiment using plastic
explosive no. 4 . These agreed well with the results. Overall, symmetrical
undisturbed scalable shock waves can be generated with the setup. Only
the reproducibility, which is comparatively poor to open shock tubes due
to the influence of wind, had to be improved.
Shock waves or shocks are a supersonic phenomenon in which the flow variables change abruptly in a thin layer. These occur with super sonic flow, such as the supersonic flight of airplanes or rockets or with explosions.
As the pressure, temperature and density change in a shock, this can be recorded. The most commonly used approach is the use of pressure sensors. Pressure information is only available at the certain locations where the sensors are installed. Any body, such as free-standing sensors, that is introduced into the flow, distorts it. Therefore, not inverse measurement methods for measuring flow variables, such as the background orientated schlieren (BOS) method or the partical image velocimetry (PIV), are used.
For this reason, a BOS setup was carried out in an open field at the Test Site Technical Safety (TTS) of BAM using a shock wave generator to visualize the shocks that result from a gas explosion. These investigations are presented in this paper. The aim is also to draw conclusions about the pressure change caused by the shock and the advantages that such a simple structure provides to the tests.
In industriellen Prozessanlagen können Druckwellen bei unfallbedingten Ereignissen (z. B. Detonation oder Bersten von Druckbehältern) schwere Schäden verursachen. Die Norm EN ISO 4126 beschreibt daher Druckentlastungseinrichtungen, die in solchen Fällen wirksam eingreifen. Dabei entweicht das Gas nach dem Öffnen der Berstscheibe und belastet das Umfeld, wie zum Beispiel benachbarte Module oder Personal (Burgess et al 2013). Daher soll in dieser Arbeit das Strömungsfeld hinter solch einer Einrichtung betrachtet werden, um exemplarisch Daten zur Einschätzung der Gefährdung im Nahbereich hinter einer Berstscheibe zu geben.
Zu diesem Zweck wurde auf dem BAM TTS ein Versuchskonzept entwickelt, bei dem ein druckfester Autoklav (Stoßwellengenerator, SWG) als zu entlastende Anlage dient. Damit lassen sich die Ausbreitung und die Impulsübertragung von Gasen und Druckwellen sowie deren Phänomenologie am offenen Ende mit verschiedenen Gasen untersuchen. In diesem Beitrag werden die Ergebnisse eines Gemischs aus Acetylen und Sauerstoff vorgestellt. Dieses Gemisch wurde gewählt, da es hohe Explosionsdrücke und Flammentemperaturen erreicht, die mit anderen Gasgemischen kaum möglich sind und somit ein Worst-Case-Szenario darstellt. Eine solche Untersuchung wurde bereits mit Wasserstoff durchgeführt (Kuang et al. 2024).
Es wurden verschiedene Auslassgeometrien von Schutzarmaturen – etwa Entlastungsöffnungen, wie bereits von Heinrich publiziert (Heinrich et al. 1966) – untersucht, um eine fundierte Nahfeldbewertung zu ermöglichen. Die experimentellen Daten können beispielsweise zur Validierung von CFD-
Simulationen dienen und erlauben, den Einfluss von Geometrie und Umgebungsbedingungen systematisch abzubilden, und liefern praxisrelevante Daten als Basis für Leitlinien für den Explosionsschutz und die Bewertung von Störfallauswirkungen in modularen Anlagen und tragen somit zur Steigerung der Anlagensicherheit bei.
This paper presents the application of background-oriented schlieren (BOS) to obtain a quantitative characterization of shock waves from a free-field outdoor pressure relief system. A BOS setup was constructed, and an investigation was carried out to examine the influence of the background. Although critical locations in the natural background were identified, they could not be eliminated due to their large number, so an optimized random dot pattern was used instead. The evaluation method also took into account the intense radiation from the high-enthalpy gas flow. The aim was to visualize the shock wave front and reconstruct the shock wave front overpressure field. To this end, a linear calibration was performed between the optical results and those of the subsidiary pressure sensors. The estimated peak overpressures showed a good agreement with the measured values, with the BOS-based estimates slightly underpredicting the measurements. The maximum observed deviation was 8%. Therefore, this approach allows peak overpressure to be determined even at locations where no physical pressure sensors can be installed due to experimental restrictions, thereby extending the measurement capability of the experimental setup.
The shock wave generator (SWG) is used to investigate the effects of blasts on humans and structures. Since its explosion characteristics deviate from the ideal characteristics in the form of excessively high impulse, various sensors were used to gain more detailed insights into the combustion and fluid mechanics inside the SWG. Two symmetrically arranged pressure sensors enabled the analysis of the almost identical but slightly shifted propagation of the shock waves inside the SWG, which differs by a few microseconds . The fluid then flows out of the SWG. In this way, it is detected in a smaller pipe section by a pressure sensor and a fast heat flux sensor. The innovative measurement technology used in this process enabled the detection of extremely high heat fluxes of over 100 MW/m² with dynamics in the range of MHz, thus allowing the local boundary layer development to be determined. After less than 100 microseconds, it changed from a laminar flow to a turbulent boundary layer. In addition, the combination of both sensors allows conclusions to be drawn about the non-ideal shock wave characteristics outside the SWG, i.e. in the area where the models to be investigated are positioned. This makes it possible to identify additional shock waves emerging from the SWG, providing valuable information for further developing and optimising the test setup.