Relating in situ gas measurements to the surface outgassing properties of cometary nuclei

The sensitivity of the gas flow field to changes in different initial conditions has been studied for the case of a highly simplified cometary nucleus model. The nucleus model simulated a homogeneously outgassing sphere with a more active ring around an axis of symmetry. The varied initial conditions were the number density of the homogeneous region, the surface temperature, and the composition of the flow (varying amounts of H2O and CO2) from the active ring. The sensitivity analysis was performed using the Polynomial Chaos Expansion (PCE) method. Direct Simulation Monte Carlo (DSMC) was used for the flow, thereby allowing strong deviations from local thermal equilibrium. The PCE approach can be used to produce a sensitivity analysis with only four runs per modified input parameter and allows one to study and quantify non-linear responses of measurable parameters to linear changes in the input over a wide range. Hence the PCE allows one to obtain a functional relationship between the flow field properties at every point in the inner coma and the input conditions. It is for example shown that the velocity and the temperature of the background gas are not simply linear functions of the initial number density at the source. As probably expected, the main influence on the resulting flow field parameter is the corresponding initial parameter (i.e. the initial number density determines the background number density, the temperature of the surface determines the flow field temperature, etc.). However, the velocity of the flow field is also influenced by the surface temperature while the number density is not sensitive to the surface temperature at all in our model set-up. Another example is the change in the composition of the flow over the active area. Such changes can be seen in the velocity but again not in the number density. Although this study uses only a simple test case, we suggest that the approach, when applied to a real case in 3D, should assist in identifying the sensitivity of gas parameters measured in situ by, for example, the Rosetta spacecraft to the surface boundary conditions and vice versa.

Revisiting the ISN Flow Parameters, using a variable IBEX pointing strategy

The Interstellar Boundary Explorer (IBEX) has observed the interstellar neutral (ISN) gas flow over the past 6 yr during winter/spring when the Earth's motion opposes the ISN flow. Since IBEX observes the interstellar atom trajectories near their perihelion, we can use an analytical model based upon orbital mechanics to determine the interstellar parameters. Interstellar flow latitude, velocity, and temperature are coupled to the flow longitude and are restricted by the IBEX observations to a narrow tube in this parameter space. In our original analysis we found that pointing the spacecraft spin axis slightly out of the ecliptic plane significantly influences the ISN flow vector determination. Introducing the spacecraft spin axis tilt into the analytical model has shown that IBEX observations with various spin axis tilt orientations can substantially reduce the range of acceptable solutions to the ISN flow parameters as a function of flow longitude. The IBEX operations team pointed the IBEX spin axis almost exactly within the ecliptic plane during the 2012-2014 seasons, and about 5° below the ecliptic for half of the 2014 season. In its current implementation the analytical model describes the ISN flow most precisely for the spin axis orientation exactly in the ecliptic. This analysis refines the derived ISN flow parameters with a possible reconciliation between velocity vectors found with IBEX and Ulysses, resulting in a flow longitude lambda∞ = 74.°5 ± 1.°7 and latitude beta∞ = -5.°2 ± 0.°3, but at a substantially higher ISN temperature than previously reported.

Interstellar Flow and Temperature Determination with IBEX: Robustness and Sensitivity to Systematic Effects

The Interstellar Boundary Explorer (IBEX) samples the interstellar neutral (ISN) gas flow of several species every year from December through late March when the Earth moves into the incoming flow. The first quantitative analyses of these data resulted in a narrow tube in four-dimensional interstellar parameter space, which couples speed, flow latitude, flow longitude, and temperature, and center values with approximately 3° larger longitude and 3 km s⁻¹ lower speed, but with temperatures similar to those obtained from observations by the Ulysses spacecraft. IBEX has now recorded six years of ISN flow observations, providing a large database over increasing solar activity and using varying viewing strategies. In this paper, we evaluate systematic effects that are important for the ISN flow vector and temperature determination. We find that all models in use return ISN parameters well within the observational uncertainties and that the derived ISN flow direction is resilient against uncertainties in the ionization rate. We establish observationally an effective IBEX-Lo pointing uncertainty of ±0°18 in spin angle and confirm an uncertainty of ±0°1 in longitude. We also show that the IBEX viewing strategy with different spin-axis orientations minimizes the impact of several systematic uncertainties, and thus improves the robustness of the measurement. The Helium Warm Breeze has likely contributed substantially to the somewhat different center values of the ISN flow vector. By separating the flow vector and temperature determination, we can mitigate these effects on the analysis, which returns an ISN flow vector very close to the Ulysses results, but with a substantially higher temperature. Due to coupling with the ISN flow speed along the ISN parameter tube, we provide the temperature Tvisn∞=8710+440/-680 K for Visn∞=26 km s⁻¹ for comparison, where most of the uncertainty is systematic and likely due to the presence of the Warm Breeze.

Multi-fluid Eulerian model of an electrospray in a host gas.

An Eulerian multifluid model is used to describe the evolution of an electrospray plume and the flow induced in the surrounding gas by the drag of the electrically charged spray droplets in the space between an injection electrode containing the electrospray source and a collector electrode. The spray is driven by the voltage applied between the two electrodes. Numerical computations and order-of-magnitude estimates for a quiescent gas show that the droplets begin to fly back toward the injection electrode at a certain critical value of the flux of droplets in the spray, which depends very much on the electrical conditions at the injection electrode. As the flux is increased toward its critical value, the electric field induced by the charge of the droplets partially balances the field due to the applied voltage in the vicinity of the injection electrode, leading to a spray that rapidly broadens at a distance from its origin of the order of the stopping distance at which the droplets lose their initial momentum and the effect of their inertia becomes negligible. The axial component of the electric field first changes sign in this region, causing the fly back. The flow induced in the gas significantly changes this picture in the conditions of typical experiments. A gas plume is induced by the drag of the droplets whose entrainment makes the radius of the spray away from the injection electrode smaller than in a quiescent gas, and convects the droplets across the region of negative axial electric field that appears around the origin of the spray when the flux of droplets is increased. This suppresses fly back and allows much higher fluxes to be reached than are possible in a quiescent gas. The limit of large droplet-to-gas mass ratio is discussed. Migration of satellite droplets to the shroud of the spray is reproduced by the Eulerian model, but this process is also affected by the motion of the gas. The gas flow preferentially pushes satellite droplets from the shroud to the core of the spray when the effect of the inertia of the droplets becomes negligible, and thus opposes the well-established electrostatic/inertial mechanism of segregation and may end up concentrating satellite droplets in an intermediate radial region of the spray.

Tridimensional simulation of the speed, pressure and turbulence fields of the air flow on the geometry of a freight truck inside a wind tunnel

This study shows the air flow behavior through the geometry of a freight truck inside a AF6109 wind tunnel with the purpose to predict the speed, pressure and turbulence fields made by the air flow, to decrease the aerodynamic resistance, to calculate the dragging coefficient, to evaluate the aerodynamics of the geometry of the prototype using the CFD technique and to compare the results of the simulation with the results obtained experimentally with the “PETER 739 HAULER” scaled freight truck model located on the floor of the test chamber. The Geometry went through a numerical simulation process using the CFX 5,7. The obtained results showed the behavior of the air flow through the test chamber, and also it showed the variations of speed and pressure at the exit of the chamber and the calculations of the coefficient and the dragging force on the geometry of the freight truck. The evaluation of the aerodynamics showed that the aerodynamic deflector is a device that helped the reduction the dragging produced in a significant way by the air. Furthermore, the dragging coefficient and force on the prototype freight truck could be estimated establishing an incomplete similarity.

Reconciliação de dados de uma malha de gasodutos.

O trabalho aborda a aplicação da técnica de reconciliação de dados para o balanço da movimentação de gás natural em uma malha de escoamento de gás não processado, elaborando também um método de cálculo rápido de inventário de um duto. Foram aplicadas, separadamente, a reconciliação volumétrica à condição padrão de medição e a reconciliação mássica, bem como realizadas comparações dos resultados em relação ao balanço original e verificação do balanço resultante de energia em termos de poder calorífico superior. Dois conjuntos de pesos foram aplicados, um arbitrado de acordo com o conhecimento prévio da qualidade do sistema de medição de cada um dos pontos, outro baseado no inverso da variância dos volumes diários apurados no período. Ambos apresentaram bons resultados e o segundo foi considerado o mais apropriado. Por meio de uma abordagem termodinâmica, foi avaliado o potencial impacto, ao balanço, da condensação de parte da fase gás ao longo do escoamento e a injeção de um condensado de gás natural não estabilizado por uma das fontes. Ambos tendem a impactar o balanço, sendo o resultado esperado um menor volume, massa e energia de fase gás na saída. Outros fatores de considerável impacto na qualidade dos dados e no resultado final da reconciliação são a qualidade da medição de saída do sistema e a representatividade da composição do gás neste ponto. O inventário é calculado a partir de uma regressão que se baseia em um regime permanente de escoamento, o que pode apresentar maior desvio quando fortes transientes estão ocorrendo no último dia do mês, porém a variação de inventário ao longo do mês possui baixo impacto no balanço. Concluiu-se que a reconciliação volumétrica é a mais apropriada para este sistema, pois os dados reconciliados levam os balanços mássicos e de energia em termos de poder calorífico, ambos na fase gás, para dentro do perfil esperado de comportamento. Embora um balanço volumétrico nulo apenas da fase gás não seja por si só o comportamento esperado quando se considera os efeitos descritos, para desenvolver um balanço mais robusto é necessário considerar as frações líquidas presentes no sistema, agregando maior dificuldade na aquisição e qualidade dos dados.

Estudo do processo de absorção e dessorção de CO2 na solução aquosa de metildietanolamina e piperazina.

Estudou-se o processo de absorção e dessorção de CO2 em solução aquosa da mistura de metildietanolamina (MDEA) e piperazina (PZ). Os ensaios de absorção foram realizados numa coluna de parede molhada com promotor de película, e, os ensaios de dessorção num sistema de semibatelada, ambos em escala de laboratório. Os testes experimentais de absorção foram realizados a 298 K e pressão atmosférica, com vazão de gás (CO2 e ar atmosférico) de 2,2.10-4 m3 s-1 e as seguintes vazões de líquido: 1,0.10-6; 1,3.10-6 e 1,7.10-6 m3 s-1. O sistema de absorção foi caracterizado através da determinação da área interfacial, a, o coeficiente volumétrico de transferência de massa, kGa, e o coeficiente volumétrico global médio de transferência de massa, KGa. No caso dos ensaios de dessorção, estes foram realizados nas temperaturas de 353, 363 e 368 K, onde empregou-se uma solução carbonatada de 10% PZ-20% MDEA e uma corrente de ar atmosférico nas vazões de 1,1.10-5 m3 s-1 e 2,7.10-5 m3 s-1. Este sistema foi caracterizado através da determinação do coeficiente volumétrico global de transferência de massa, KLa. Os resultados experimentais da área interfacial mostram que este é função da vazão do líquido, sugerindo uma maior área de irrigação como o aumento desta, onde teve-se uma maior área de transferência de massa. O resultado do parâmetro, KGa, indica uma dependência da vazão de líquido, a qual está associada à variação da área interfacial e à dependência do parâmetro KG com o perfil das concentrações da MDEA e PZ ao longo da coluna. A partir da teoria do duplo filme e pelo conhecimento dos parâmetros KGa, a e kGa, estimou-se um parâmetro cinético-difusivo associado à fase líquida, (( ) ) . Os resultados experimentais mostram que esse parâmetro varia pouco com a vazão de líquido, indicando tratar-se de um processo independente da hidrodinâmica do líquido, característico de sistemas com reação rápida. A concentração das aminas e carbamatos, nos ensaios de absorção e dessorção, foi determinada através dos modelos de calibração obtidas pela técnica de espectroscopia no infravermelho. Nos ensaios de absorção, foram observados que a concentração de PZ teve uma variação considerável (4 a 5% massa massa-1), entanto que a de MDEA variou pouco (0,3 a 0,5% massa massa-1), sugerindo que o processo de absorção de CO2 na mistura MDEA-PZ é controlado principalmente pela PZ, e supõe-se que a MDEA tem um papel de receptor de prótons procedentes da reação entre a PZ e o CO2. Nos ensaios de dessorção, observou-se que esse processo é afetado pela temperatura, sendo que, em temperaturas perto da ebulição (372 K), a taxa de dessorção de CO2 é maior do que em temperaturas menores, em certa forma é devido à dependência da velocidade de reação química com a temperatura. Os resultados do parâmetro KLa indicam que este diminui em função da concentração de carbamato de PZ (por exemplo, na temperatura de 368 K, de 7,5.10-4 a 1,0.10-4 s-1), devido a que este componente é decomposto em altas temperaturas gerando o CO2 e as aminas, sugerindo uma diminuição na velocidade de dessorção de CO2. Assim também, os resultados experimentais do parâmetro KLa indicam que este aumenta ligeiramente com a vazão do gás.

Breaking the boundaries. The transformation of Central European gas markets. OSW Point of View Number 46, December 2014

According to the European Council decision of February 2011, the process of creating the European Union’s internal gas market should be completed by the end of 2014. Therefore, it is worth summarising the changes which have taken place in the gas markets of Central Europe so far. The past few years have seen not only a period of gradual ‘marketisation’ of the national gas sectors, but also the building of new gas infrastructure, a redrawing of the gas flow map, and changes in the ownership of the Central European gas companies. Another change in Central Europe is the fact that individual states and companies are moving away from their traditional focus on their national gas markets; instead, they are beginning to develop a variety of concepts for the regional integration of Central European markets. This publication attempts to grasp the main elements of the ongoing transformation of Central Europe’s gas markets, with particular emphasis on the situation in Poland, the Czech Republic, Slovakia and Hungary.

The Contribution of the Activation Entropy to the Gas-Phase Stability of Modified Nucleic Acid Duplexes

Tricyclo-DNA (tcDNA) is a sugar-modified analogue of DNA currently tested for the treatment of Duchenne muscular dystrophy in an antisense approach. Tandem mass spectrometry plays a key role in modern medical diagnostics and has become a widespread technique for the structure elucidation and quantification of antisense oligonucleotides. Herein, mechanistic aspects of the fragmentation of tcDNA are discussed, which lay the basis for reliable sequencing and quantification of the antisense oligonucleotide. Excellent selectivity of tcDNA for complementary RNA is demonstrated in direct competition experiments. Moreover, the kinetic stability and fragmentation pattern of matched and mismatched tcDNA heteroduplexes were investigated and compared with non-modified DNA and RNA duplexes. Although the separation of the constituting strands is the entropy-favored fragmentation pathway of all nucleic acid duplexes, it was found to be only a minor pathway of tcDNA duplexes. The modified hybrid duplexes preferentially undergo neutral base loss and backbone cleavage. This difference is due to the low activation entropy for the strand dissociation of modified duplexes that arises from the conformational constraint of the tc-sugar-moiety. The low activation entropy results in a relatively high free activation enthalpy for the dissociation comparable to the free activation enthalpy of the alternative reaction pathway, the release of a nucleobase. The gas-phase behavior of tcDNA duplexes illustrates the impact of the activation entropy on the fragmentation kinetics and suggests that tandem mass spectrometric experiments are not suited to determine the relative stability of different types of nucleic acid duplexes.

Flow of gases through beds of broken solids,

At head of title: United States Department of commerce. R.P. Lamont, secretary. Bureau of Mines. Scott Turner, director.

On one-dimensional channel flow in the presence of a magnetic field.

"Prepared for the Air Force Ballistic Missile Division, Headquarters Air Research and Development Command, under contract AF 04(647)-309 advanced propulsion systems."

Mass flow measurement techniques for a flight enthalpy probe. Contract no. P.O.33-531174-G48.

Mode of access: Internet.

Chemical kinetics in a reentry flow field, by M. H. Bortner.

At head of title: Space Sciences Laboratory. Aerophysics Section.

An analysis of nonequilibrium inviscid flow,

"Air Force contract no. AF40(600)-928."

Principles and practice of flow meter engineering

Includes bibliography.