An attempt to predict spray characteristics at early stage of the atomization process by using surface density and curvature distribution

Author(s):  
L. Palanti ◽  
S. Puggelli ◽  
L. Langone ◽  
A. Andreini ◽  
J. Reveillon ◽  
...  
Author(s):  
Mohamed Soltan ◽  
Buthaina Al Abdulla ◽  
AlReem Al Dosari ◽  
Kumaran Kannaiyan ◽  
Reza Sadr

Dispersion of nanoparticles in pure fuels alters their key fuel physical properties, which could affect their atomization process, and in turn, their combustion and emission characteristics in a combustion chamber. Therefore, it is essential to have a thorough knowledge of the atomization characteristics of nanofuels (nanoparticles dispersed in pure fuels) to better understand their latter processes. This serves as the motivation for the present work, which attempts to gain a good understanding of the atomization process of the alternative, gas-to-liquid (GTL), jet fuel based nanofuels. The macroscopic spray characteristics such as spray cone angle, liquid sheet breakup, and liquid sheet velocity are determined by employing shadowgraph imaging technique. The effect of nanoparticles weight concentration and ambient pressures on the spray characteristics are investigated in a high pressure-high temperature constant volume spray rig. To this end, a pressure swirl nozzle with an exit diameter of 0.8 mm is used to atomize the fuels. The macroscopic spray results demonstrate that the nanoparticles dispersion at low concentrations affect the near nozzle region. The spray liquid sheet breakup distance is reduced by the presence of nanoparticle due to the early onset of disruption in the liquid sheet. Consequently, the liquid sheet velocity in that spray region is higher for nanofuels when compared to that of pure fuels. Also, the ambient pressure has a significant effect on the spray features as reported in the literature.


2021 ◽  
Vol 220 (4) ◽  
Author(s):  
Rie Ayukawa ◽  
Seigo Iwata ◽  
Hiroshi Imai ◽  
Shinji Kamimura ◽  
Masahito Hayashi ◽  
...  

Nucleation of microtubules (MTs) is essential for cellular activities, but its mechanism is unknown because of the difficulty involved in capturing rare stochastic events in the early stage of polymerization. Here, combining rapid flush negative stain electron microscopy (EM) and kinetic analysis, we demonstrate that the formation of straight oligomers of critical size is essential for nucleation. Both GDP and GTP tubulin form single-stranded oligomers with a broad range of curvatures, but upon nucleation, the curvature distribution of GTP oligomers is shifted to produce a minor population of straight oligomers. With tubulin having the Y222F mutation in the β subunit, the proportion of straight oligomers increases and nucleation accelerates. Our results support a model in which GTP binding generates a minor population of straight oligomers compatible with lateral association and further growth to MTs. This study suggests that cellular factors involved in nucleation promote it via stabilization of straight oligomers.


2010 ◽  
Vol 22 (1) ◽  
pp. 225
Author(s):  
M. Romek ◽  
B. Gajda ◽  
M. Rolka ◽  
Z. Smorag

Preimplantation pig embryos undergo modifications in their metabolism. Glucose is metabolized via aerobic and anaerobic pathways at early cleavage stages, whereas glycolysis becomes the dominant pathway as development progresses. Moreover, fatty acid oxidation rate increases significantly at the early blastocyst stage. It is possible that mitochondria undergo structural and functional changes in response to altering embryo metabolism. Therefore, the aim of this study was to estimate changes in surface density of inner mitochondrial membranes (Sv) and mitochondrial activity (Av) per unit volume of mitochondria during the maturation of oocyte and early development of porcine embryos derived in vivo. The measurements were carried out on immature and matured oocytes, zygotes, 4 to 8 cell embryos, morula, blastocysts, and late and hatched blastocysts (10 to 39 embryos per stage). To estimate Sv, material was stained with mixture of 1.05 μM 10-N-nonyl Acridine Orange (NOA) and 0.5 μM Mito Tracker Deep Red (MtDR) for 30 min at 20°C. To measure Av, oocytes and embryos were labeled sequentially with 0.5μM Mito Tracker Orange CMTMRos (MtOR) for 30 min at 39°C and 0.5 μM MtDr for 30 min at 20°C. Embryos were then fixed in 3.8% formaldehyde and analyzed by confocal microscopy with a LSM 510 Meta Zeiss. The amounts of fluorescence emitted from embryos labeled as INOA, IMtOR, and IMtDR were measured because these ratios were directly proportional to Sv and Av, respectively. Values Sv and Av calculated for embryos at different stages of development were compared by ANOVA and Tukey’s intervals. During oocyte maturation, Av was low and remained unchanged, whereas Sv significantly decreased (P < 0.05) from 0.26 ± 0.021 f.a.u. (fluorescence arbitrary units) at immature oocytes to 0.11 ± 0.012 f.a.u. at matured oocytes. From the zygote to morula stage, Av was constant and then increased almost 5 times to the value of 0.95 ± 0.036 f.a.u. at the blastocyst stage, whereas late and hatched blastocyst characterized by significantly lower (P < 0.001) Av: 0.51 ± 0.023 and 0.34 ± 0.019 f.a.u., respectively. Surface density of the inner mitochondrial membrane in pig embryo during cleavage significantly (P < 0.05) increased from 0.16 ± 0.013 f.a.u. at zygote to 0.35 ± 0.020 and 0.75 ± 0.059 f.a.u. at morula and blastocyst, respectively. In conclusion, during the early stage of pig embryo development, mitochondria undergo structural and functional changes. Results demonstrate that the area density of inner mitochondrial membranes increases earlier (at 4 to 8 cell stages) than mitochondrial activity, which increase not before blastocyst stage. Furthermore, after blastocoel formation, when energy requirement is significantly lower, Av decrease but Sv remain constant.


2000 ◽  
Vol 11 (7) ◽  
pp. 2359-2371 ◽  
Author(s):  
Eugenia Leikina ◽  
Leonid V. Chernomordik

Fusion mediated by influenza hemagglutinin (HA), a prototype fusion protein, is commonly detected as lipid and content mixing between fusing cells. Decreasing the surface density of fusion-competent HA inhibited these advanced fusion phenotypes and allowed us to identify an early stage of fusion at physiological temperature. Although lipid flow between membranes was restricted, the contacting membrane monolayers were apparently transiently connected, as detected by the transformation of this fusion intermediate into complete fusion after treatments known to destabilize hemifusion diaphragms. These reversible connections disappeared within 10–20 min after application of low pH, indicating that after the energy released by HA refolding dissipated, the final low pH conformation of HA did not support membrane merger. Although the dynamic character and the lack of lipid mixing at 37°C distinguish the newly identified fusion intermediate from the intermediate arrested at 4°C described previously, both intermediates apparently belong to the same family of restricted hemifusion (RH) structures. Because the formation of transient RH structures at physiological temperatures was as fast as fusion pore opening and required less HA, we hypothesize that fusion starts with the formation of multiple RH sites, only a few of which then evolve to become expanding fusion pores.


Author(s):  
J. Eckstein ◽  
E. Freitag ◽  
C. Hirsch ◽  
T. Sattelmayer ◽  
R. von der Bank ◽  
...  

The low frequency response of the spray from a generic air-blast diffusion burner with a design typical of an engine system has been investigated as part of an experimental study to describe the combustion oscillations of aero engine combustors called rumble. The atomization process was separated from the complex instability mechanism of rumble by using sinusoidal forcing of the air mass flow rate without combustion. Pressure drop across the burner and the velocity on the burner exit were found to follow the steady Bernoulli equation. Phase-locked PIV measurements of the forced velocity field of the burner show quasi-steady behavior of the air flow field. The phase-locked spray characteristics were measured for different fuel flow rates. Here again quasi-steady behavior of the atomization process was observed. With combustion, the phase-locked Mie-scattering intensity of the spray cone was found to follow the spray behavior measured in the non-combusting tests. These findings lead to the conclusion that the unsteady droplet SMD mean and amplitude of the air-blast atomizer can be calculated using the steady state atomization correlations with the unsteady burner air velocity.


Author(s):  
Shenghao Yu ◽  
Bifeng Yin ◽  
Shuai Wen ◽  
Xifeng Li ◽  
Hekun Jia ◽  
...  

The early stage spray characteristics have a great impact on the secondary atomization progress, and thus affectthe engine combustion and emission performances. The experimental investigation of the early stage spray behaviors with biodiesel and diesel was carried out by employing a laser-based Mie-scattering method. The results show that the spray tip penetration for biodiesel is higher than that for diesel at the early stage spray under the same injection pressure. Moreover, the early stage spray tip penetration can be longer under high injection pressures for two fuels. Besides, the early stage spray cone angle for biodiesel is narrower than that for diesel, and the spray cone angle is especially higher than biodiesel by 25.8% after start of injection time of 0.01ms. Furthermore, under the same injection condition, the difference of early stage spray area between diesel and biodiesel is not obvious, while the spray volume for biodiesel is larger than that for diesel, and also the sprayvolume can be enlarged by increasing injection pressure for both fuels.DOI: http://dx.doi.org/10.4995/ILASS2017.2017.4651


2021 ◽  
Author(s):  
Thomas Christou ◽  
Björn Stelzner ◽  
Nikolaos Zarzalis

Abstract In order to meet the higher requirements for clean combustion technology in aircraft engine applications and thus reduce harmful emissions, especially nitrogen oxide emissions, the major jet engine manufacturers are developing lean premixed prevaporized (LPP) combustors that operate at very high pressure. In this context, thermoacoustic instabilities may occur within the combustion chamber. The unsteady heat released by the flame generates pressure waves, which are coupled to the inlet air velocity by a feedback loop. This loop amplifies the instabilities of the inlet air velocity, which in turn influences the atomization process. Since the atomization process at the airblast atomizers of most jet engine combustors determines critical operating characteristics such as air-to-fuel ratio (AFR), flame stability, or NOx emissions, predicting the performance of this process under unsteady conditions has a significant value. The present experimental study focuses on the influence of oscillating airflows on the spray characteristics at the airblast atomization process. The experimental setup was based on a two-dimensional prefilmer where a water film flow was introduced on one surface. The airflow was excited by a siren, whereby an excitation frequency near 94 Hz was investigated. The airflow oscillation under this excitation frequency was characterized using a Constant Temperature Anemometer (CTA), while the generated spray was investigated with a Phase Doppler Anemometry (PDA) system. The spray was investigated in a variety of positions along the radial axis, providing spatial information, apart from temporal. The characterization of the spray via PDA includes a two-component droplet velocity detection and diameter measurement, while the spray mass flux for each measured position was also calculated. The acquired data were phase averaged via an in-house developed processing algorithm, while through a statistical analysis the confidence intervals of the calculations were included. The excitation frequency strongly influenced all spray characteristics, namely, the Sauter Mean Diameter (SMD), the droplet velocities, the mass flux, as well as the local air-to-liquid ratio (ALR). Depending on the phase angle, the size distribution of the spray changes, explaining the observed oscillating behavior of the spray characteristics.


Author(s):  
Fathollah Ommi ◽  
Ehsan Movahednejad ◽  
S. Mostafa Hosseinalipour ◽  
Chien-Pin Chen

The distribution of sizes and velocities of droplets initially formed in sprays is an important piece of information needed in the spray modeling, because it defines the initial condition of the spray droplets in the predictive calculations of the downstream flow fields. The early stage of the atomization process (Primary Breakup) is clearly deterministic, whereas the droplet formation stage is random and stochastic. The stochastic aspect deals with the stage of droplet formation after the liquid bulk breakup by statistical means through the maximum entropy principle (MEP) based. The MEP provided model predicts atomization process while satisfying constrain equations of mass, momentum and energy. This model is capable for considering drag force on droplets downstream through a gas field. The model prediction is compared favorably with the experimentally measured size and velocity distribution for droplets, near the liquid bulk breakup region, produced by an air-blast annular nozzle. Therefore, the present model can be used to predict the initial droplet size and velocity distribution in droplet formation region of sprays.


2005 ◽  
Vol 127 (2) ◽  
pp. 301-306 ◽  
Author(s):  
J. Eckstein ◽  
E. Freitag ◽  
C. Hirsch ◽  
T. Sattelmayer ◽  
R. von der Bank ◽  
...  

The low-frequency response of the spray from a generic airblast diffusion burner with a design typical of an engine system has been investigated as part of an experimental study to describe the combustion oscillations of aeroengine combustors called rumble. The atomization process was separated from the complex instability mechanism of rumble by using sinusoidal forcing of the air mass flow rate without combustion. Pressure drop across the burner and the velocity on the burner exit were found to follow the steady Bernoulli equation. Phase-locked particle image velocimetry measurements of the forced velocity field of the burner show quasisteady behavior of the air flow field. The phase-locked spray characteristics were measured for different fuel flow rates. Here again quasi-steady behavior of the atomization process was observed. With combustion, the phase-locked Mie-scattering intensity of the spray cone was found to follow the spray behavior measured in the noncombusting tests. These findings lead to the conclusion that the unsteady droplet Sauter mean diameter mean and amplitude of the airblast atomizer can be calculated using the steady-state atomization correlations with the unsteady burner air velocity.


Aerospace ◽  
2021 ◽  
Vol 8 (9) ◽  
pp. 249
Author(s):  
Sim Sing Mei ◽  
Aslina Anjang Ab Rahman ◽  
Mohd Shukur Zainol Abidin ◽  
Nurul Musfirah Mazlan

A comparison of d2 law and penetration length of biofuels with Jet–A through the incorporation of fuel properties and actual combustor inlet data at various flight trajectories is presented. This study aims to identify fuel properties and flight operating conditions that most influence droplet characteristics accurately. The study comprises two phases involving a simulation using GSP to predict combustor inlet data for the respective flight operating conditions and a simulation using ANSYS Fluent V18.1 to obtain combustion characteristics of biofuels and Jet–A . The biofuels chosen in this study are Jatropha Bio-synthetic Paraffinic Kerosene (JSPK) and Camelina Bio-synthetic Paraffinic Kerosene (CSPK), evaluated as pure (100%) and blend (50%) with Jet–A. Thrust specific fuel consumption (TSFC) of biofuels is improved due to lower fuel consumed by the engine. The d2 law curve shows a heat-up period that takes place at the early stage of the combustion process. The penetration length of the fuels is shorter at take-off. Combusting biofuels reduce combustion temperature and the penetration length of the droplet.


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