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Real-gas Effects on Fluid Injection: a Numerical and Experimental study. – REFINE

Real-gas Effects on Fluid Injection: a Numerical and Experimental study.

The present proposal concerns the propulsion with application to the automotive and aerospace science and technology. The need for higher efficiency and lower emission levels leads to increase pressure i.e. to reach supercritical properties of fluids. The objective of REFINE is to build a simple well-controlled test-bench able to study a fluid injection under sub-, trans- and super-critical conditions and to associate experimental and numerical diagnostics to deliver the finest information.

High pressure jet study

Mixing is one of the most important phenomena in combustion devices because it determines combustion efficiency and stability along with heat transfer characteristics. In addition, most of the current understanding of turbulence and mixing is the result of atmospheric-pressure studies providing numerous numerical and experimental databases are available. A similar work has to be undertaken for sub-, trans- and super-critical flows investigation, i.e. real-gas effects have to be considered. Indeed, this research field lacks of indisputable experimental data, useful for the numerical code validation. Simulation has made serious progress in the last decade but still need well-documented experimental test cases. Actually, only few experimental test- benches are able to reach/run supercritical cases. Three are located in the USA (Pennsylvania State Univ., Univ. of Florida and AFRL), two in Germany (M51 and P8 at DLR) and one in France at ONERA (Mascotte). Except facilities from Univ. of Florida, they are all running hot fire configurations dedicated to rocket issues that already are highly complex systems. In addition, no convincing experimental data are available. The declared objective of REFINE is to fill out this need by the mean of simple well-defined experimentations with very advanced diagnostics to deliver the finest information. To achieve this objective, two French Labs, CORIA – UMR6614 and GREMI – UMR7344, are associated as ‘ANR’ partners. In addition, ISL (Institut Saint-Louis) will be associated as sub-contractor. REFINE addresses then Basic Research. These investigations should provide a better understanding of atomization, mixing and flow dynamics for high-pressure subcritical and supercritical jets. It is expected that these studies will also lead to an enhancement of physical models, which will be used for achieving an improved design methodology.

Numerical and experimental diagnostics will be performed in order to deliver the most suitable information (density, velocity, spreading angle for example). To achieve it and have comparable diagnostics, X-ray measures should provide non-polluted information that will be associated to shadowgraphy, CBOS (Colored Background Oriented Schlieren) and numerical LES.
- Shadowgraphy is a line-of-sight method that is often used to obtain qualitative and quantitative information in injection applications. Using a short exposure time light source, detailed information on the interaction between the jet and the surrounding gas can be obtained.
- The use of X-ray based techniques could offer an alternative solution to conventional optical techniques such as LIF, PIV, LDA, etc. that may be perturbed by an index gradient. The X-ray measurements to be performed for the jet characterization in the REFINE project consist in radiography, i.e. absorption measurement, using a table top soft X-ray source associated with a dedicated X-ray detector to collect digital radiographs.
- Evidence of the CBOS technique has already been done in the case of supersonic flows. The relevance of this technique in the scope of super-critical conditions will be tested. The CBOS method, an extension of the Schlieren method, allows refractive objects to be visualized by their distortion of a colored patterned background.
- Numerical simulations (LES) will be performed as diagnostics with the numerical solver SiTCom-B. It is a structured LES and DNS compressible multi-species Navier- Stokes code with perfect or real gas thermodynamics and immersed boundary methods (IBM).

Ongoing results.

Short time: REFINE test bench running and validation of first results.

An invited conference has been done by G. Ribert during the Vth Int. Combustion Institute Summer School (ICISS) in Brazil (2015). The topic was dedicated to the real-gas injection phenomenon.

The REFINE project focuses on the experimental investigation and numerical simulation of real-fluid injection and mixing processes under sub-, trans- and super-critical conditions. The domain of interest of the present proposal concerns the propulsion with application to the automotive and aerospace science and technology where supercritical fluids may be considered as propellants. Indeed, the need for higher efficiency and lower emission levels leads to increase pressure and temperature levels, i.e. to reach supercritical properties of fluids. The objective of REFINE is to build a simple well-controlled test-bench able to study a fluid injection under sub-, trans- and super-critical conditions and to associate experimental and numerical diagnostics to deliver the finest information. An ethane injection occurs in a 5-liter high-pressure experimental test-bench. The X-ray diagnostics setting-up will be the project keystone, as it allows for delivering a non-polluted density measurement. Indeed, such diagnostics are not disrupted by the index gradient observed in corrugated flows, contrary to laser techniques. Colored background oriented Schlieren visualization is used for backup as well as a more classical shadowgraphy technique. Numerical simulations will be realized in parallel to consolidate physics understanding and for model validation.

Project coordination

Guillaume RIBERT (COmplexe de Recherche Interprofessionnel en Aérothermochimie) – ribert@coria.fr

The author of this summary is the project coordinator, who is responsible for the content of this summary. The ANR declines any responsibility as for its contents.

Partner

GREMI Groupe de Recherches sur l'Energétique des Milieux Ionisés
CORIA COmplexe de Recherche Interprofessionnel en Aérothermochimie

Help of the ANR 469,909 euros
Beginning and duration of the scientific project: December 2013 - 48 Months

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