Abstract

PurposeThe purpose of this paper is to present a procedure to design an experimental setup meant to validate an innovative approach for simulating, via computational fluid dynamics, a high-pressure gas release from a rupture (e.g. on an offshore oil and gas platform). The design is based on a series of scaling exercises, some of which are anything but trivial.Design/methodology/approachThe experimental setup is composed of a wind tunnel, the instrumented scaled (1:10) mock-up of an offshore platform and a gas release system. A correct scaling approach is necessary to define the reference speed in the wind tunnel and the conditions of the gas release to maintain similarity with respect to the real-size phenomena. The scaling of the wind velocity and the scaling of the gas release were inspired by the approach proposed by Hall et al. (1997): a dimensionless group was chosen to link release parameters, wind velocity and geometric scaling factor.FindingsThe theoretical scaling approaches for each different part of the setup were applied to the design of the experiment and some criticalities were identified, such as the existence of a set of case studies with some release parameters laying outside the applicability range of the developed scaling methodology, which will be further discussed.Originality/valueThe resulting procedure is one of a kind because it involves a multi-scaling approach because of the different aspects of the design. Literature supports for the different scaling theories but, to the best of the authors’ knowledge, fails to provide an integrated approach that considers the combined effects of scaling.

Highlights

  • The Deepwater Horizon accident in the Gulf of Mexico is dated back to year 2010

  • In this work, we describe a scaling procedure used to perform reduced-scale experiments to reproduce high-pressure accidental gas releases in open industrial environments

  • Scaling laws for subsonic gas releases or gas dispersion have been well addressed in numerous past works and related literature, but some additional issues arise when the gas leakage produces a supersonic jet

Read more

Summary

Introduction

The Deepwater Horizon accident in the Gulf of Mexico is dated back to year 2010. Since many initiatives have been carried out to prevent similar or even less impacting events on© Alberto Moscatello, Anna Chiara Uggenti, Gaetano Iuso, Domenic D’Ambrosio, Gioacchino Cafiero, Raffaella Gerboni and Andrea Carpignano. A scaling procedure strongly depends on the identification of the main physical phenomena that characterise the flow-field to be experimentally reproduced in a different scale This identification is introduced, detailed and discussed in the case study reported hereafter. Because of the strong expansion in the discharge ambient, the jet accelerates up to a supersonic velocity (Mach number, Ma ) 1), but after a certain distance, a normal shock occurs and the velocity immediately drops down to a subsonic value; this normal shock region is called Mach disk (Franquet et al, 2015) This region is characterised by high discontinuities in all the flow field variables. The time scales involved are of the order of approximately 10 m s, that is, the time necessary for the Mach disk complete development (Tang et al, 2017)

Objectives
Methods
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call