Hot wire anemometer response in a flow with acoustic disturbances

The response of a hot wire to acoustic disturbances in a low velocity flow is considered, taking account of disturbances in flow temperature, density, velocity and pressure. It is shown that operation at a fixed wire temperature requires that contributions other than that due to velocity disturbances alone have a net effect which increases with mean flow speed. Elimination of the effects of pressure, density and temperature disturbances so that the wire indicates only the velocity disturbance of the acoustic wave may be achieved by operating the wire at a selected temperature. This optimal wire temperature decreases as the mean flow velocity increases.     

Phase transitions in materials with thermal memory

A model for thermally induced phase transitions in materials with thermal memory is explored. From a general starting point of the thermodynamics of materials with memory, field equations with an order parameter, temperature and temperature gradient are derived. The heat flux is given by an integral over the history of the temperature gradient. Asymptotic analysis yields that to leading order, there is a relation connecting the discontinuity in the temperature field with the normal velocity of the transition zone. The temperature discontinuity is negligible for low transition zone velocity. The latent heat must depend on velocity and becomes negligible compared with the specific heat as the normal velocity approaches the speed of propagation of thermal disturbances. There is also a condition which is different from the Stefan condition connecting discontinuities in the temperature gradient with velocity, but reduces to this form, under certain approximations, in the low transition zone velocity limit. The circumstances where the transition zone velocity may exceed the speed of thermal disturbances are discussed.     

Phase transitions in materials with thermal memory: The case of unequal conductivities

A model for thermally induced phase transitions in materials with thermal memory was recently proposed, where the equations determining heatflow were assumed to be the same in both phases. In this work, the model is generalized to the case of phase dependent heatflow relations. The temperature (or coldness) gradient is decomposed into two parts, each zero on one phase and equal to the temperature (or coldness) gradient on the other. However, they vary smoothly over the transition zone. These are treated as separate independent quantities in the derivation of field equations from thermodynamics. Heat flux is given by an integral over the history of the temperature gradient, with different kernels on each phase. Asymptotic analysis is carried out to obtain generalizations of previous results. These involve the jump in temperature across the transition zone and the normal derivatives of the temperature on each phase boundary, which are related to the velocity of the transition zone and a latent heat dependent on this velocity, as well as the speeds of thermal disturbances in the two phases.     

一维过驱动爆轰波形成的数值研究

利用有限速率的基元反应模型对一维过驱动爆轰波的形成过程进行数值模拟.研究表明,在上游高温、高压、高速来流作用下首先会形成一道强激波,其波面方存在诱导区和放热区,然后诱导区和放热区界面会在来流扰动的作用下发生失稳,经过复杂的波系运动过程形成过驱动爆轰波.通过对不同初始条件下界面失稳过程的模拟和分析,研究了混合气体的组元、温度,来流的压力、温度、速度对过驱动爆轰波形成的影响.     

A narrowband single-mode dye laser

The linewidth of a cw-single-mode tunable dye laser has been investigated. It was found that the linewidth is determined by microscopic velocity fluctuations of the turbulent flow within the dye cell of the laser and by fluctuations of the pump power. The linewidth is further influenced by mechanical disturbances and by temperature fluctuations of the dye solution. The results of the investigations made it possible to achieve a reduction of the velocity fluctuations. It is shown that under adequate operating conditions the free-running dye laser has a linewidth of 2 MHz.     

INVESTIGATION OF BOILING OF REFRIGERATING MEDIUM UNDER CONDITIONS OF IMPULSE DISTURBANCES

This article describes investigations of bubbly boiling in flow of a refrigerating medium under conditions of impulse disturbances occurring in refrigeration engineering systems. The development and decay of boiling is induced by impulsively changing parameters, such as pressure and mass flux density, of the two-phase system in a tubular channel. It is confirmed that the two-phase systems exhibit wave properties and the induced disturbances propagate with a finite velocity. Correlations are elaborated to evaluate the propagation velocity of disturbance signals during the development and decay of boiling in a coil tube. Investigations are conducted by feeding under pressure a heat exchanger with an environment-friendly refrigerant R404A.     

Self-Similar Gas Motion Near The Evaporating Electrode of An Electric Arc

Simple solutions of 1Dt gas-dynamical equations based on similarity analysis are possible for the gas surrounding a point source of mass and energy such as an electrode (cathode) arc spot. To obtain nontrivial (non-zero temperature) solutions throughout, two-scale formulation is used that permits an additional boundary condition near the source. Three generalised gas flow variables, R, Z and V, related to gas density, temperature and velocity are calculated and presented as functions of a single similarity parameter, λ, related to position and time. The computational results are compared with data from two gas discharge experiments: on gas disturbances due to an electric arc of micrometer length in atmospheric air and on expansion of a metal-vapour plasma cloud generated by a low-pressure cold-cathode arc.     

A simple and efficient levitation technique for noncontact coating of inertial confinement fusion targets

A simple and very efficient gas jet levitation technique for levitating inertial confinement fusion (ICF) targets has been developed. A low velocity gas jet through diverging nozzle generates precisely controlled low Reynolds number flow pattern, capable of levitating polymer microballoons up to 2500 μm diameter. Different shaped diverging nozzle are investigated, satisfactory levitation is achieved with simple conical shapes. With this setup microballoon can be levitated for hours with excellent stability, continuous rotation and at the desired height (reproducible with in less than 100 μm). The height of stabilization depends upon cone angle of diverging nozzle and velocity of levitating gas. This technique is very robust and highly insensitive to external disturbances like nonuniform temperature fields and vibrations. This setup is very economical to fabricate, easy to operate and can be used efficiently in various spray coating application involving plastic and metallic layers on microballoons.     

FEM for Blood-Based SWCNTs Flow Through a Circular Cylinder in a Porous Medium with Electromagnetic Radiation

This work aims to study magnetohydrodynamic flow through a circular cylinder in a horizontal position of SWCNTs in blood as a base fluid in the existence of non-linear thermal radiation and heat source/sink. Three kinds of nanoparticles shapes are considered. The study is employed the finite element technique to explore and enhance the influences of essential parameters on temperature profiles and is debated the heat transport within blood injects with SWCNTs and exposes to electromagnetic radiation. The treatment with thermal analysis and heat transfer rate being a better substitute more than surgery and chemotherapy for cancer therapy. Utilizing of nanoparticles thermal features is a mounting area of nanomedicine field because of the probable for purposeful demolition of cancer cells.This remedy is relied on many parameters, including nanofluid thermal conductivity, nanoparticles volume fraction,thermal radiation and power and heat source. The numerical solutions for flow and heat transfer features are assessed for diverse governing parameters values. The obtained results are substantiated against the relevant numerical results in the published researches. Results show that both flow velocity and temperature increase for larger values of thermal radiation, heat source and SWCNTs volume fraction with lamina and cylinder shapes. Also, spherical shape of SWCNTs occurs high disturbances in velocity and temperature distribution in the case of cooled cylinder.     

Wave motion of incompressible turbulent fluid

Evolution of small disturbances in a fully developed incompressible turbulent flow is considered on the base of the transport equation for the single-point probability density function (PDF) of velocity fluctuations. It is shown that at high frequencies this equation is similar to the Vlasov equation for charged plasma in a self-consistent electromagnetic field having longitudinal wave solutions for turbulent stresses similar to Langmuir waves. It is found that the longitudinal waves of turbulent stresses have a constant phase velocity and can be damped, neutral, or growing waves, depending on the type of undisturbed probability density function of velocity fluctuations. The obtained result differs from the previously published solutions to this problem using the statistical moments closures according to which the wave disturbances should be neutral or damped. The possibilities of experimental observation of longitudinal waves of turbulent stresses are analyzed.     

Velocity of a perturbation in infinite lattice systems

The problem of defining and estimating the velocity of disturbances in a crystal is investigated. Some results are given for plane rotors and anharmonic systems.Research partially supported by CNR.     

Radiative Instability of an Unbounded Jet Flow

The problem of the linear dynamics of disturbances of an unbounded jet flow with a piecewise linear velocity profile is considered. The stable disturbances of a flow in an incompressible medium are so-called flow waves localized near a vorticity jump. In this work, it is shown that the amplitudes of these waves slowly increase in a compressible medium due to acoustic radiation; i.e., an instability appears. The asymptotic solution to the problem for small Mach numbers is represented in terms of Airy functions. An analytic expression for the growth increment of the disturbances is obtained.     

Aerothermodynamic Analysis of a Reentry Brazilian Satellite

This work deals with a computational investigation on the small ballistic reentry Brazilian vehicle SAtélite de Reentrada Atmosférica (SARA). Hypersonic flows over the vehicle SARA at zero-degree angle of attack in chemical equilibrium and thermal nonequilibrium are modeled by the direct simulation Monte Carlo method, which has become the main technique for studying complex multidimensional rarefied flows, and which properly accounts for the nonequilibrium aspects of the flows. The emphasis of this paper is to examine the behavior of the primary properties during the high-altitude portion of SARA reentry. In this way, velocity, density, pressure, and temperature field are investigated for altitudes of 100, 95, 90, 85, and 80?km. In addition, comparisons based on geometry are made between axisymmetric and planar two-dimensional configurations. Some significant differences between these configurations were noted on the flowfield structure in the reentry trajectory. The analysis showed that the flow disturbances have different influence on velocity, density, pressure, and temperature along the stagnation streamline ahead of the capsule nose. It was found that the stagnation region is a thermally stressed zone. It was also found that the stagnation region is a zone of strong compression, high wall pressure. Wall pressure distributions are compared with those of available experimental data, and good agreement is found along the spherical nose for the altitude range investigated.     

On stability of channel flow of thermoviscous fluid

The paper presents key results on a large-scale entrainment of thermoviscous liquid layers with different temperatures and their further mixing observed in the plane-parallel flow with an inflectional velocity profile. We show that the instability development in the channel is more intensive at the inflection point vicinity and is not related directly to vorticity generation in the near-wall region. The considered flow being unstable relative to the finite-amplitude harmonic disturbances possesses several resonant frequencies initiating the most intense entrainment. Temperature fields are analyzed based on the time-averaged entrainment layer thickness and temperature isoline displacement. We discuss the spectral properties of flow enstrophy, vorticity, and kinetic energy in terms of asymptotics of cascades observed and coherent structures. Okubo-Weiss criterion is used for mapping of four flow zones wherein an active filamentation of the turbulent veil or long-term existence of vortex structures is possible.     

Stability of time-periodic flow with laminar boundary-layer separation

The influence of the low-frequency modulation of flow behind a rectangular backward-facing step on the amplitude characteristics of disturbances in the separated laminar boundary layer has been studied. The experimental data were obtained by the method of hot-wire anemometry in a wind tunnel at a low subsonic velocity. Response of the separated flow to the long-wave oscillations generated by a local source of disturbances on the surface of the experimental model was clarified. The low-frequency nonstationarity of the separation region leads to a growth of velocity fluctuations in the separated boundary layer, which dominate the laminar-turbulent transition and the state of the flow in the near-wall region.     

Dynamical Characteristics of Traveling Wave Packets of Total Electron Content Disturbances

Using the COPHASE method and the GPS interferometry method for travelling ionospheric disturbances, we analyze in detail the spatio-temporal properties of travelling wave packets (TWP) of total electron content (TEC) disturbances. The analysis is performed on the example of a clearest TWP manifestation observed in California, USA, in October 18, 2001, using the GLOBDET technique, developed at the Institute of Solar-Terrestrial Physics of the Siberian Branch of RAS for global detection and monitoring of natural and technogenic ionospheric disturbances on the basis of TEC variations retrieved from the global network of GPS receivers. In the time domain, TWPs are quasi-periodic TEC oscillations of duration about 1 h, period of 10–20 min, and amplitude exceeding that of the background TEC fluctuations by at least one order of magnitude. The velocity and direction of TWP motion are similar to those of mid-latitude mesoscale travelling ionospheric disturbances, as obtained earlier from the analysis of phase parameters of HF radio signals and the signals of geostationary satellites and discrete space radio sources.     

Investigation of Boiling of Refrigeration Medium Under Periodic Disturbance Conditions

Abstract

Experimental investigations of boiling in flow of a refrigeration medium under disturbances typically occurring in refrigeration units are conducted. The development and decay of boiling is stimulated by periodic changes of mass flux density in the coil tube. It is confirmed that the two-phase systems exhibit wave properties and the disturbances generated in the system propagate with finite velocities. An experiment-based correlation to describe the disturbance propagation velocity during the development and decay of boiling in the coil tube is elaborated. The investigations are carried out for an environment-friendly refrigerant R404A supplied under pressure to the heat exchanger.     

DNS of rotating and non-rotating turbulent flows with synthetic inlet conditions

In this paper, direct numerical simulations (DNS) are presented to understand the effects of the inlet conditions on the turbulent energy decay rate of isotropic turbulence. A perfect control of the inlet conditions cannot be achieved in realistic simulations reproducing the effects of a solid grid, which, on the other hand, is possible by adding to a uniform inlet velocity U ₀ analytical anisotropic single- or multiple-scale velocity disturbances. The single-scale simulations with different disturbances with a wave number κ show a scaling of the turbulent energy q versus x ₁/M with M=2π/κ. The energy decay rate m for multiple-scale disturbances is decreased compared to the case with single-scale disturbances. The transition from anisotropic to isotropic turbulence is analysed through the evolution of the statistics, in particular, those linked to the flow structures. Flow visualisations of the vorticity field and joint of the velocity components at different distances from the inlet illuminate the reasons for the differences between single- and multiple-scale disturbances. The reduction of m, for the latter, indicates the way to generate isotropic turbulence at high microscale R _λ. Simulations at different rates of solid-body rotation aligned with the streamwise direction were also performed for the flows with multiple- and single-scale disturbances. Variations of the rotation rate Ω allow to investigate the modifications of the vortical structures for single-scale disturbances. At N _Ω=2ΩL/U ₀=10, the comparison between single- and multiple-scale disturbances shows a further increase of R _λ in the latter flow. One-dimensional energy spectra at different distances from the inlet indicate when the effects of the inlet disturbances disappear. Good agreement, in the inertial and in the exponential decay ranges, between the present spectra and those from the DNS of forced isotropic turbulence demonstrates the quality of the numerical method used.     

Secondary instability of a swept-wing boundary layer disturbed by controlled roughness elements

Abstract  

Wind-tunnel data on velocity perturbations evolving in a laminar swept-wing flow under low subsonic conditions are reported. The focus of the present experiments are secondary disturbances of the boundary layer which is modulated by stationary streamwise vortices. Both the stationary vortices and the secondary oscillations of interest are generated in a controlled manner. The experimental data are obtained through hot-wire measurements. Thus, evolution of the vortices, either isolated or interacting with each other, is reconstructed in detail. As is found, the secondary disturbances, initiating the laminar-flow breakdown, are strongly affected by configuration of the stationary boundary-layer perturbation that may have an implication to laminar–turbulent transition control.