4.7 Article

Single-Droplet Combustion of Jet A-1, Hydroprocessed Vegetable Oil, and Their Blends in a Drop-Tube Furnace

期刊

ENERGY & FUELS
卷 35, 期 9, 页码 7232-7241

出版社

AMER CHEMICAL SOC
DOI: 10.1021/acs.energyfuels.0c03476

关键词

-

资金

  1. Fundacao para a Ciencia e Tecnologia (FCT) [UID/EMS/50022/2019, UIDB/50022/2020]

向作者/读者索取更多资源

The study examined the combustion characteristics of different fuel mixtures in a drop-tube furnace, revealing that the composition of the mixtures influences the fuel characteristics. The 75% JF mixture at higher temperatures exhibited increased burning rates, likely due to puffing and microexplosions.
The environmental impact and the dependence upon fossil fuels in the aeronautical sector have promoted the demand for alternative and greener fuels. The implementation of alternative fuels is one of the main challenges for this sector in the near future. A possible short-term solution might be the blending of biofuels with jet fuel, which would allow for the use of greener fuels and a reduction in the greenhouse gases and pollutant emissions without significant changes in the existing fleets of the companies, with the purpose to develop a drop-in fuel. In this context, this work examines the combustion characteristics of single droplets of Jet A-1 (JF), hydroprocessed vegetable oil (NExBTL), and their mixtures in a drop-tube furnace (DTF). The objective of this work is to evaluate the influence of the mixture composition on the fuel characteristics. Droplets with diameters of 155 +/- 5 mu m, produced by a commercial droplet generator, were injected into the DTF, whose wall temperature and oxygen concentration were controlled. Experiments were conducted for three temperatures (900, 1000, and 1100 degrees C). The combustion of droplets was evaluated through the images obtained with a high-speed camera coupled with a high magnification lens and an edge detection algorithm. From the images allowed for the analysis of droplet combustion, data are reported for the temporal evolution of droplet sizes and burning rates. The results revealed that the mixtures followed the D-2 law, except the mixture with 75% JF for a DTF wall temperature of 1100 degrees C. The 75% JF mixture did not follow the D-2 law as a result of the occurrence of puffing and microexplosions, which enhanced the burning rates. Additionally, it was observed that the mixtures with a higher content of JF present brighter flames and higher burning rates.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.7
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

Article Green & Sustainable Science & Technology

Sustainable aviation fuels and imminent technologies - CO2 emissions evolution towards 2050

Ivo Abrantes, Ana F. Ferreira, Andre Silva, Mario Costa

Summary: The aviation industry has promoted various approaches to reduce CO2 emissions, including improving aircraft technology and using sustainable low-carbon fuels. However, achieving carbon-neutral growth and a 50% reduction in net emissions by 2050 compared to 2005 levels will require a combination of imminent aircraft technologies with a higher introduction of Sustainable Aviation Fuel (SAF). Results show that these goals cannot be met solely by the current strategies, and carbon-neutral growth may only be possible by 2040 with the right combination of technologies and SAF introduction rates.

JOURNAL OF CLEANER PRODUCTION (2021)

Article Mechanics

Influence of wetting behavior on the morphology of droplet impacts onto dry smooth surfaces

P. Foltyn, D. Ribeiro, A. Silva, G. Lamanna, B. Weigand

Summary: This study systematically investigates the role of surface wettability on the morphology of droplet impacts, highlighting its significant influence on the receding phase. Through visualization of different wetting behaviors, it is found that decreasing wettability leads to higher receding rates, impacting the maximum spreading diameter as well.

PHYSICS OF FLUIDS (2021)

Article Engineering, Aerospace

Contribution to the physical description of supercritical cold flow injection: The case of nitrogen

Leandro B. Magalhaes, Andre R. R. Silva, Jorge M. M. Barata

Summary: This study focuses on evaluating gas jet topology for different injector conditions using the Reynolds-averaged Navier-Stokes equations, predicting the axial density decay in supercritical nitrogen jets based on the thermal breakup mechanism concept. The results provide a better understanding of the available experimental data.

ACTA ASTRONAUTICA (2022)

Article Engineering, Aerospace

Dynamics of a gyrostat satellite with the vector of gyrostatic moment tangent to the orbital plane

Renato H. Morais, Luis F. F. M. Santos, Andre R. R. Silva, Rui Melicio

Summary: This paper investigates the equilibria, bifurcation of equilibria, and asymptotic stability conditions of a gyrostat satellite in a circular orbit with its gyrostatic moment tangent to the orbital plane and collinear with the orbital speed. The study reveals interesting results regarding the bifurcation of equilibria when the gyrostat angular momentum is aligned with any of the orbital coordinate frames. A symbolic-numerical method is used to obtain polynomial equations for equilibria positions, and the asymptotic stability is tested using the Lyapunov stability theory scheme.

ADVANCES IN SPACE RESEARCH (2022)

Article Astronomy & Astrophysics

Short-Term Consequences of Asteroid Impacts into the Ocean: A Portuguese Case Study

Renato H. Morais, Luis F. F. M. Santos, Andre R. R. Silva, Rui Melicio

Summary: This study expands knowledge about asteroid impacts in the ocean and their regional environmental consequences. It evaluates the consequences of three asteroid impacts and finds that tsunami waves are the most threatening and influential effect.

UNIVERSE (2022)

Article Mechanics

Influence of wetting behavior on the morphology of droplet impacts onto dry-patterned micro-structured surfaces

P. Foltyn, D. Ribeiro, A. Silva, G. Lamanna, B. Weigand

Summary: The influence of regularly patterned micro-structures on the physical outcomes of droplet impacts is not well understood. This study systematically investigates the morphology of such surfaces and finds that the outcomes of droplet impacts depend on the impact energy, surface wettability, and structure dimensions. The study also discovers that roughness features can both trigger and inhibit splashing, and identifies reproducible arrangements of air entrapment within the structure.

PHYSICS OF FLUIDS (2022)

Article Mechanics

Criterion for bubble encapsulation on drop impact onto a liquid film

D. Ribeiro, A. R. R. Silva, M. R. O. Panao

Summary: The phenomenon of bubble encapsulation occurs when droplets impact a liquid film under specific conditions, but there is currently no established criterion for predicting its onset. Visualization of the phenomenon from two perspectives, the common lateral perspective and a bottom perspective, provides insights into the dynamics and formation mechanisms. The bottom shadowgraphs show capillary wavy patterns and perturbations in the liquid film, suggesting a significant role in the onset of bubble encapsulation. The criterion for the onset of bubble encapsulation is based on drop characteristics and properties in the Reynolds number and liquid film thickness and thermophysical properties in the Ohnesorge number.

PHYSICS OF FLUIDS (2023)

Article Engineering, Aerospace

Computational characterization of the temperature field in coaxial nitrogen injection under supercritical conditions

Leandro B. Magalhaes, Andre R. R. Silva, Jorge M. M. Barata

Summary: This document addresses the modeling of fluids in the supercritical regime, specifically in liquid-propelled rocket engines. Nitrogen is used as a surrogate for oxygen-hydrogen mixture to investigate turbulence mixing without combustion and chemical reactions. The temperature field validation for nitrogen coaxial injection at supercritical conditions is crucial for the stable operation of liquid rocket motors.

ACTA ASTRONAUTICA (2023)

Article Thermodynamics

The impact of temperature on heated liquid films: Crater and jetting impact dynamics

Daniel A. Vasconcelos, Andre R. R. Silva, Jorge M. M. Barata

Summary: This study evaluates the influence of liquid film temperature on crater and jet dynamics. The results show that temperature differences promote the formation of recirculation zones near the impact surface and the crater boundaries, as well as influence the shape and curvature of the crater.

EXPERIMENTAL THERMAL AND FLUID SCIENCE (2023)

Article Mechanics

Insights on bubble encapsulation after drop impact on thin liquid films

Daniela F. S. Ribeiro, Miguel R. O. Panao, Jorge M. M. Barata, Andre R. R. Silva

Summary: The goal of this study is to investigate the mechanism of bubble encapsulation when a drop impacts a thin liquid film. The results show that the mechanism consists of two stages. In the first stage, the drop impacts the liquid film, causing a prompt splash and a crown splash. The collapsing crown-bounding rim encapsulates air, forming a bubble. In the second stage, three different phenomena of bubble encapsulation can occur. The study also examines the first perturbation imposed by the drop impact and proposes an empirical correlation for its propagation velocity. Additionally, the geometry of the bubble is investigated.

INTERNATIONAL JOURNAL OF MULTIPHASE FLOW (2023)

Article Engineering, Aerospace

Optimal leading-edge deflection for flapping airfoil propulsion

Emanuel A. R. Camacho, Andre R. R. Silva, Flavio D. Marques

Summary: This paper investigates the aerodynamic characteristics of oscillating airfoils, comparing the performance of a modified version of the NACA0012 with the standard flapping method. By employing a gradient-based optimization method, the study identifies pitching amplitudes that maximize propulsive power and efficiency. The results indicate that the proposed flapping method shows more potential and achieves higher thrust, with near-optimal efficiency, compared to conventional methods.

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING (2023)

Article Engineering, Aerospace

Influence of a Deflectable Leading-Edge on a Flapping Airfoil

Emanuel A. R. Camacho, Flavio D. Marques, Andre R. R. Silva

Summary: The present study focuses on the importance of leading-edge dynamic incidence in the propulsive performance of flapping airfoils. By adding a pitching leading-edge to a conventional NACA0012 airfoil, the propulsive characteristics can be improved. Numerical results show that the leading-edge pitching amplitude greatly affects the propulsive power and efficiency, providing significant improvements.

AEROSPACE (2023)

Article Engineering, Aerospace

Supercritical Injection Modeling by an Incompressible but Variable Density Approach

Leandro B. Magalhaes, Andre R. R. Silva, Jorge M. M. Barata

Summary: Supercritical nitrogen jet behavior is simulated using a variable density approach, considering heat transfer in the injector. The proposed methodology's suitability for simulating supercritical injection behavior is validated through comparisons with experimental data and compressible formulations from the literature.

AEROSPACE (2023)

Proceedings Paper Engineering, Aerospace

Satellite Star Tracker Breadboard with Space Debris Detection Capability for LEO

Joel Filho, Paulo Gordo, Nuno Peixinho, Ricardo Gafeira, Rui Melicio, Andre Silva

Summary: This paper evaluates the possibility of running space debris algorithms on a star tracker device. A breadboard prototype was developed and tested, and a dual-purpose star tracker with stars detection and optical debris detection capability is proposed. This research is of major importance as it addresses the need for detecting space debris.

12TH EASN INTERNATIONAL CONFERENCE ON INNOVATION IN AVIATION & SPACE FOR OPENING NEW HORIZONS (2023)

Article Engineering, Aerospace

Description of a Eulerian-Lagrangian Approach for the Modeling of Cooling Water Droplets

Ruben Meireles, Leandro Magalhaes, Andre Silva, Jorge Barata

Summary: This paper presents a tool developed in-house for modeling free-falling water droplet cooling processes, utilizing a two-way coupling model and stochastic separated flow technique. The study focuses on the interactions between water droplets and carrier fluid at different humidity ratios, with consideration for heat and mass transfer coefficients and vibrations.

AEROSPACE (2021)

暂无数据